+2010-03-10 Sampo Niskanen
+
+ * Released version 1.0.0
+ * [BUG] Removing point of freeform fin could create intersecting shape
+
+2010-03-09 Sampo Niskanen
+
+ * Updated thrustcurves with newest curves from thrustcurve.org
+ * Updated splash screen
+
2010-03-05 Sampo Niskanen
* [BUG] Fixed exception for fins with small root chord
+OpenRocket 1.0.0 (2010-03-10):
+-------------------------------
+
+Added numerous new motor thrustcurves from thrustcurve.org, and fixed
+a few more bugs.
+
+
OpenRocket 0.9.6 (2010-02-17):
-------------------------------
Must-have:
-- Go through thrust curves and select best ones
-- Updated splash screen
-- BUG: Invalid fin points possible when removing points
Maybe:
Memory usage:
+- Store data as floats instead of doubles
- Reduce memory leakage when closing windows
- Make simulation data immutable, don't store copies in undo/redo
- Profile memory usage during operation (send data to server?)
+- Warn user when 90% of memory is used, offer to send info to server
Logging:
Motor support:
+- Combine duplicates into one display in the selection dialog
+ - A single manufacturer/designation can contain multiple thrust curves
+ - Delays are combined
+ - Type is selected based on any not-unknown type
+ - Hybrid type always includes P delay
+ - Default delay selected based on heuristics
+ - Store recently used motors, use in default selection
- Integration with thrustcurve.org (syncing?)
- Reading thrust curves from external directory
- Plot motor thrust curve
UI issues:
+- Easy/intuitive zooming of plots
- Only schedule rocket figure update instead of each time updating it
- Importing flight data (file/altimeter)
- Saving as SVG
- Simulate other branches
- Remove need for 5m launch rod in real-time simulations (reduces apogee)
A simulation listener that checks when sufficient velocity has been reached?
+- [BUG] Take single-fin cant yaw effect into account
Structural analysis:
exponential growth until time step is reached (t1 = 1.5*t0)
- Limit time step during while on launch rod
- Re-investigate 15% reduction of three-fin CNa
-In 0.9.7:
+In 1.0.0:
- BUG: Simulation table max. acceleration takes into account parachute deceleration
+- Go through thrust curves and select best ones
+- Updated splash screen
+- BUG: Invalid fin points possible when removing points
# The OpenRocket build version
-build.version=0.9.7pre
+build.version=1.0.0
# The source of the package. When building a package for a specific
<?xml version='1.0' encoding='utf-8'?>
-<openrocket version="1.0" creator="OpenRocket 0.9.6">
+<openrocket version="1.0" creator="OpenRocket 0.9.7pre">
<rocket>
<name>A simple model rocket</name>
<designer>Sampo Niskanen</designer>
<clusterrotation>0.0</clusterrotation>
<motormount>
<motor configid="da326836-0959-4c94-bcd5-49dee07235a4">
+ <type>single</type>
<manufacturer>Estes</manufacturer>
<designation>A8</designation>
<diameter>0.018</diameter>
<delay>3.0</delay>
</motor>
<motor configid="05896b5a-71a7-48ac-b7ae-eadeb267975b">
+ <type>single</type>
<manufacturer>Estes</manufacturer>
<designation>B4</designation>
<diameter>0.018</diameter>
<delay>4.0</delay>
</motor>
<motor configid="b13e8ca2-f54d-4ca8-9b23-06c6c9eb237a">
+ <type>single</type>
<manufacturer>Estes</manufacturer>
<designation>C6</designation>
<diameter>0.018</diameter>
<delay>3.0</delay>
</motor>
<motor configid="e1dc7488-77c0-403a-b54f-c01db07aba2f">
+ <type>single</type>
<manufacturer>Estes</manufacturer>
<designation>C6</designation>
<diameter>0.018</diameter>
<delay>5.0</delay>
</motor>
<motor configid="5d9a2765-395d-4d9c-9678-38eed0988c72">
+ <type>single</type>
<manufacturer>Estes</manufacturer>
<designation>C6</designation>
<diameter>0.018</diameter>
<atmosphere model="isa"/>
<timestep>0.05</timestep>
</conditions>
- <flightdata maxaltitude="47.129" maxvelocity="28.806" maxacceleration="141.16" maxmach="0.084639" timetoapogee="3.3349" flighttime="15.158" groundhitvelocity="3.9886">
+ <flightdata maxaltitude="47.294" maxvelocity="28.75" maxacceleration="141.23" maxmach="0.084475" timetoapogee="3.3507" flighttime="15.081" groundhitvelocity="4.3477">
<databranch name="Main" types="Time,Altitude,Vertical velocity,Vertical acceleration,Total velocity,Total acceleration,Position upwind,Position parallel to wind,Lateral distance,Lateral direction,Lateral velocity,Lateral acceleration,Angle of attack,Roll rate,Pitch rate,Yaw rate,Mass,CP location,CG location,Stability margin calibers,Mach number,Reynolds number,Thrust,Drag force,Drag coefficient,Axial drag coefficient,Friction drag coefficient,Pressure drag coefficient,Base drag coefficient,Normal force coefficient,Pitch moment coefficient,Yaw moment coefficient,Side force coefficient,Roll moment coefficient,Roll forcing coefficient,Roll damping coefficient,Pitch damping coefficient,Reference length,Reference area,Vertical orientation (zenith),Lateral orientation (azimuth),Wind velocity,Air temperature,Air pressure,Speed of sound,Simulation time step,Computation time">
<event time="0" type="launch"/>
<event time="0" type="ignition"/>
<event time="0.09" type="liftoff"/>
<event time="0.24" type="launchrod"/>
- <event time="0.73493" type="burnout"/>
- <event time="3.3849" type="apogee"/>
- <event time="3.7349" type="ejectioncharge"/>
- <event time="3.7349" type="recoverydevicedeployment"/>
- <event time="15.158" type="groundhit"/>
- <event time="15.158" type="simulationend"/>
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</flightdata>
</simulation>
<?xml version='1.0' encoding='utf-8'?>
-<openrocket version="1.0" creator="OpenRocket 0.9.6">
+<openrocket version="1.0" creator="OpenRocket 0.9.7pre">
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<comment>Edit the "Clustered Inner Tube" and see the "Cluster" tab for clustering options.</comment>
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- <motorconfiguration configid="5d9a2765-395d-4d9c-9678-38eed0988c72"/>
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<motormount>
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+ <type>single</type>
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<delay>3.0</delay>
</motor>
<motor configid="05896b5a-71a7-48ac-b7ae-eadeb267975b">
+ <type>single</type>
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<delay>4.0</delay>
</motor>
<motor configid="b13e8ca2-f54d-4ca8-9b23-06c6c9eb237a">
+ <type>single</type>
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<delay>3.0</delay>
</motor>
<motor configid="e1dc7488-77c0-403a-b54f-c01db07aba2f">
+ <type>single</type>
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<diameter>0.018</diameter>
<delay>5.0</delay>
</motor>
<motor configid="5d9a2765-395d-4d9c-9678-38eed0988c72">
+ <type>single</type>
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+ <flightdata maxaltitude="47.917" maxvelocity="28.744" maxacceleration="143.95" maxmach="0.084456" timetoapogee="3.3612" flighttime="11.553" groundhitvelocity="6.2116">
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</databranch>
</flightdata>
</simulation>
<atmosphere model="isa"/>
<timestep>0.05</timestep>
</conditions>
- <flightdata maxaltitude="262.5" maxvelocity="91.257" maxacceleration="186.33" maxmach="0.26839" timetoapogee="5.7127" flighttime="48.779" groundhitvelocity="6.1509">
- <warning>Recovery device deployment at high speed (25.8 m/s).</warning>
+ <flightdata maxaltitude="262.23" maxvelocity="91.431" maxacceleration="186.3" maxmach="0.26891" timetoapogee="5.6854" flighttime="48.568" groundhitvelocity="6.1546">
+ <warning>Recovery device deployment at high speed (25.9 m/s).</warning>
<databranch name="Main" types="Time,Altitude,Vertical velocity,Vertical acceleration,Total velocity,Total acceleration,Position upwind,Position parallel to wind,Lateral distance,Lateral direction,Lateral velocity,Lateral acceleration,Angle of attack,Roll rate,Pitch rate,Yaw rate,Mass,CP location,CG location,Stability margin calibers,Mach number,Reynolds number,Thrust,Drag force,Drag coefficient,Axial drag coefficient,Friction drag coefficient,Pressure drag coefficient,Base drag coefficient,Normal force coefficient,Pitch moment coefficient,Yaw moment coefficient,Side force coefficient,Roll moment coefficient,Roll forcing coefficient,Roll damping coefficient,Pitch damping coefficient,Reference length,Reference area,Vertical orientation (zenith),Lateral orientation (azimuth),Wind velocity,Air temperature,Air pressure,Speed of sound,Simulation time step,Computation time">
<event time="0" type="launch"/>
<event time="0" type="ignition"/>
<event time="0.07" type="liftoff"/>
<event time="0.2" type="launchrod"/>
- <event time="1.8874" type="burnout"/>
- <event time="4.8874" type="ejectioncharge"/>
- <event time="4.8874" type="recoverydevicedeployment"/>
- <event time="5.7637" type="apogee"/>
- <event time="48.779" type="groundhit"/>
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- <datapoint>9.2789,242.77,-6.2417,-0.097833,6.1931,0.13828,6.4133,0.0020408,6.4133,3.1821e-4,1.973,0.097728,NaN,NaN,NaN,NaN,0.23738,NaN,NaN,NaN,0.018246,289637,0,2.3072,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9596,286.55,98441,339.42,0.5,0.43759</datapoint>
- <datapoint>9.7789,239.66,-6.2121,0.059156,6.2419,0.1048,5.4159,0.0020408,5.4159,3.7681e-4,2.0163,0.086508,NaN,NaN,NaN,NaN,0.23738,NaN,NaN,NaN,0.018389,291992,0,2.3445,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0277,286.57,98478,339.43,0.5,0.43772</datapoint>
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</flightdata>
</simulation>
<atmosphere model="isa"/>
<timestep>0.05</timestep>
</conditions>
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<event time="0.07" type="liftoff"/>
<event time="0.2" type="launchrod"/>
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- <event time="7.3659" type="apogee"/>
- <event time="8.8667" type="ejectioncharge"/>
- <event time="8.8667" type="recoverydevicedeployment"/>
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</flightdata>
</simulation>
<?xml version='1.0' encoding='utf-8'?>
-<openrocket version="1.1" creator="OpenRocket 0.9.6">
+<openrocket version="1.1" creator="OpenRocket 0.9.7pre">
<rocket>
<name>Hybrid rocket with dual parachute deployment</name>
<comment>This design demonstrates a high-power hybrid rocket with dual parachute deployment. The drogue parachute is deployed at apogee and the main parachute at 200 m altitude.
<atmosphere model="isa"/>
<timestep>0.05</timestep>
</conditions>
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<event time="0" type="launch"/>
<event time="0" type="ignition"/>
<event time="3.7412" type="burnout"/>
<event time="12.141" type="apogee"/>
<event time="12.191" type="recoverydevicedeployment"/>
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- <event time="66.673" type="groundhit"/>
- <event time="66.673" type="simulationend"/>
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- <datapoint>34.119,466.77,-19.135,0.01777,19.145,0.089518,79.948,0.0059965,79.948,7.5005e-5,1.9115,0.087736,NaN,NaN,NaN,NaN,3.4209,NaN,NaN,NaN,0.056555,2356462,0,33.68,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0382,285.05,95738,338.51,0.5,1.0656</datapoint>
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- <datapoint>41.619,323.77,-19.001,0.017627,19.009,0.040453,65.742,0.0059965,65.742,9.1212e-5,1.9074,0.036411,NaN,NaN,NaN,NaN,3.4209,NaN,NaN,NaN,0.056062,2366979,0,33.679,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9595,285.98,97416,339.08,0.5,1.0678</datapoint>
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- <datapoint>43.119,295.29,-18.974,0.017954,18.984,0.098704,62.916,0.0059965,62.916,9.5309e-5,1.9196,0.097058,NaN,NaN,NaN,NaN,3.4209,NaN,NaN,NaN,0.055968,2369140,0,33.681,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0582,286.17,97750,339.19,0.5,1.0682</datapoint>
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- <datapoint>49.829,174.39,-7.3772,3.4822,7.8778,3.5298,50.138,0.0059965,50.138,1.196e-4,1.8893,0.57773,NaN,NaN,NaN,NaN,3.4209,NaN,NaN,NaN,0.023191,993155,0,45.573,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.6295,287.01,99267,339.7,0.14165,1.0732</datapoint>
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- <datapoint>39.521,870.56,-19.509,0.018624,19.519,0.036916,41.036,-0.0020125,41.036,-4.9042e-5,2.0448,0.031874,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057933,2327188,0,33.665,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9975,282.43,91212,336.92,0.5,1.1811</datapoint>
- <datapoint>40.021,860.81,-19.499,0.020559,19.513,0.19119,40.038,-0.0020125,40.038,-5.0265e-5,1.9497,0.19008,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057909,2328343,0,33.677,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.6682,282.49,91321,336.96,0.5,1.1812</datapoint>
- <datapoint>40.521,851.07,-19.49,0.017881,19.499,0.019498,39.062,-0.0020125,39.062,-5.1521e-5,1.9536,0.0077738,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057861,2328524,0,33.662,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9651,282.55,91430,337,0.5,1.1814</datapoint>
- <datapoint>41.021,841.32,-19.481,0.018556,19.49,0.064815,38.093,-0.0020125,38.093,-5.2831e-5,1.9226,0.062102,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057829,2329338,0,33.665,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.8307,282.62,91539,337.04,0.5,1.1815</datapoint>
- <datapoint>41.521,831.58,-19.472,0.018503,19.481,0.028469,37.134,-0.0020125,37.134,-5.4195e-5,1.9117,0.021636,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057794,2.33e6,0,33.664,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.8797,282.68,91647,337.07,0.5,1.1816</datapoint>
- <datapoint>42.021,821.85,-19.462,0.018659,19.472,0.038377,36.174,-0.0020125,36.174,-5.5633e-5,1.9285,0.033536,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.05776,2330754,0,33.665,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9781,282.74,91756,337.11,0.5,1.1818</datapoint>
- <datapoint>42.521,812.12,-19.453,0.018638,19.462,0.024942,35.212,-0.0020125,35.212,-5.7153e-5,1.9202,0.016574,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057725,2331453,0,33.664,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.8957,282.81,91865,337.15,0.5,1.1819</datapoint>
- <datapoint>43.021,802.4,-19.444,0.018757,19.453,0.052531,34.246,-0.0020125,34.246,-5.8766e-5,1.9448,0.049068,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057692,2332185,0,33.665,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0172,282.87,91974,337.19,0.5,1.1821</datapoint>
- <datapoint>43.521,792.68,-19.434,0.018809,19.444,0.072184,33.282,-0.0020125,33.282,-6.0468e-5,1.9099,0.069691,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057658,2332910,0,33.666,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.8071,282.93,92082,337.23,0.5,1.1822</datapoint>
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- <datapoint>44.521,773.25,-19.416,0.018234,19.425,0.018928,31.409,-0.0020125,31.409,-6.4074e-5,1.863,0.0050766,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057588,2334216,0,33.663,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.8705,283.06,92299,337.3,0.5,1.1825</datapoint>
- <datapoint>45.021,763.55,-19.406,0.018594,19.416,0.070545,30.469,-0.0020125,30.469,-6.6051e-5,1.897,0.06805,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057556,2334986,0,33.665,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9972,283.12,92408,337.34,0.5,1.1826</datapoint>
- <datapoint>45.521,753.85,-19.397,0.018934,19.408,0.11503,29.506,-0.0020125,29.506,-6.8206e-5,1.9538,0.11346,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057524,2335773,0,33.668,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.1207,283.19,92516,337.38,0.5,1.1828</datapoint>
- <datapoint>46.021,744.15,-19.388,0.018174,19.397,0.060113,28.522,-0.0020125,28.522,-7.0559e-5,1.9824,0.0573,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057487,2336321,0,33.663,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0667,283.25,92625,337.42,0.5,1.1829</datapoint>
- <datapoint>46.521,734.46,-19.379,0.018098,19.388,0.018098,27.531,-0.0020125,27.531,-7.31e-5,1.9824,2.646e-5,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057452,2336987,0,33.663,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9824,283.31,92733,337.46,0.5,1.1831</datapoint>
- <datapoint>47.021,724.77,-19.369,0.018307,19.379,0.048291,26.534,-0.0020125,26.534,-7.5846e-5,2.0048,0.044686,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057419,2337716,0,33.664,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0704,283.38,92841,337.5,0.5,1.1832</datapoint>
- <datapoint>47.521,715.09,-19.36,0.018188,19.369,0.01931,25.531,-0.0020125,25.531,-7.8826e-5,2.008,0.0064882,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057385,2338381,0,33.663,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0175,283.44,92950,337.53,0.5,1.1834</datapoint>
- <datapoint>48.021,705.41,-19.351,0.01835,19.361,0.056553,24.52,-0.0020125,24.52,-8.2075e-5,2.0347,0.053493,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057353,2339107,0,33.664,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.1132,283.5,93058,337.57,0.5,1.1838</datapoint>
- <datapoint>48.521,695.74,-19.342,0.018123,19.351,0.020004,23.502,-0.0020125,23.502,-8.5632e-5,2.039,0.0084684,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057318,2339751,0,33.663,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0514,283.56,93166,337.61,0.5,1.1839</datapoint>
- <datapoint>49.021,686.07,-19.333,0.018572,19.343,0.095315,22.494,-0.0020125,22.494,-8.9469e-5,1.9922,0.093488,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057287,2340543,0,33.666,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.8553,283.63,93274,337.65,0.5,1.1841</datapoint>
- <datapoint>49.521,676.41,-19.324,0.017887,19.333,0.017941,21.498,-0.0020125,21.498,-9.3615e-5,1.9929,0.0013885,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057251,2341094,0,33.662,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.995,283.69,93382,337.69,0.5,1.1842</datapoint>
- <datapoint>50.021,666.75,-19.315,0.018481,19.325,0.10169,20.489,-0.0020125,20.489,-9.8225e-5,2.0429,0.099992,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057221,2341908,0,33.666,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.1892,283.75,93490,337.72,0.5,1.1844</datapoint>
- <datapoint>50.521,657.09,-19.306,0.017739,19.315,0.019752,19.468,-0.0020125,19.468,-1.0337e-4,2.0386,0.0086865,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057184,2342442,0,33.661,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0259,283.82,93598,337.76,0.5,1.1845</datapoint>
- <datapoint>51.021,647.44,-19.297,0.01842,19.307,0.10712,18.436,-0.0020125,18.436,-1.0916e-4,2.0913,0.10553,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057155,2343270,0,33.666,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.2455,283.88,93706,337.8,0.5,1.1847</datapoint>
- <datapoint>51.521,637.8,-19.288,0.018163,19.298,0.10633,17.377,-0.0020125,17.377,-1.1581e-4,2.1437,0.10477,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057121,2343917,0,33.665,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.2967,283.94,93814,337.84,0.5,1.1848</datapoint>
- <datapoint>52.021,628.15,-19.278,0.018672,19.29,0.15522,16.286,-0.0020125,16.286,-1.2357e-4,2.2208,0.15409,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057091,2344732,0,33.669,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.4456,284,93921,337.88,0.5,1.185</datapoint>
- <datapoint>52.521,618.52,-19.268,0.019883,19.284,0.23726,15.205,-0.0020125,15.205,-1.3236e-4,2.1026,0.23642,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057067,2345746,0,33.678,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.7579,284.07,94029,337.91,0.5,1.1851</datapoint>
- <datapoint>53.021,608.89,-19.26,0.015993,19.268,0.020405,14.155,-0.0020125,14.155,-1.4217e-4,2.0962,0.012671,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.057015,2345620,0,33.655,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0778,284.13,94137,337.95,0.5,1.1852</datapoint>
- <datapoint>53.521,599.26,-19.251,0.018021,19.262,0.15028,13.126,-0.0020125,13.126,-1.5332e-4,2.0216,0.1492,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.056991,2346668,0,33.666,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.8044,284.19,94244,337.99,0.5,1.1854</datapoint>
- <datapoint>54.021,589.63,-19.243,0.017146,19.252,0.091077,12.126,-0.0020125,12.126,-1.6596e-4,1.9769,0.089448,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.056954,2347148,0,33.661,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.8467,284.25,94352,338.03,0.5,1.1855</datapoint>
- <datapoint>54.521,580.01,-19.234,0.017216,19.243,0.065066,11.13,-0.0020125,11.13,-1.8082e-4,2.0083,0.062747,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.056921,2347801,0,33.66,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0996,284.32,94459,338.07,0.5,1.1857</datapoint>
- <datapoint>55.021,570.4,-19.225,0.017323,19.234,0.045031,10.131,-0.0020125,10.131,-1.9865e-4,1.9875,0.041566,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.056888,2348468,0,33.66,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9271,284.38,94567,338.1,0.5,1.1858</datapoint>
- <datapoint>55.521,560.79,-19.217,0.017418,19.225,0.032204,9.1339,-0.0020125,9.1339,-2.2033e-4,2.001,0.027088,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.056856,2349140,0,33.66,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0404,284.44,94674,338.14,0.5,1.186</datapoint>
- <datapoint>56.021,551.18,-19.208,0.017946,19.218,0.099784,8.1456,-0.0020125,8.1456,-2.4706e-4,1.952,0.098157,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.056827,2349922,0,33.664,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.8095,284.5,94782,338.18,0.5,1.1861</datapoint>
- <datapoint>56.521,541.58,-19.199,0.018106,19.209,0.13175,7.186,-0.0020125,7.186,-2.8006e-4,1.8867,0.1305,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.056796,2350649,0,33.666,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.6974,284.57,94889,338.22,0.5,1.1862</datapoint>
- <datapoint>57.021,531.98,-19.19,0.017141,19.199,0.067624,6.2508,-0.0020125,6.2508,-3.2196e-4,1.854,0.065415,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.056759,2351119,0,33.66,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.7591,284.63,94996,338.26,0.5,1.1864</datapoint>
- <datapoint>57.521,522.39,-19.181,0.017168,19.19,0.044863,5.3186,-0.0020125,5.3186,-3.7839e-4,1.8747,0.041449,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.056727,2351767,0,33.66,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9348,284.69,95103,338.29,0.5,1.1865</datapoint>
- <datapoint>58.021,512.8,-19.173,0.017232,19.182,0.029308,4.3783,-0.0020125,4.3783,-4.5966e-4,1.8866,0.023707,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.056695,2352427,0,33.66,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9209,284.75,95211,338.33,0.5,1.1867</datapoint>
- <datapoint>58.521,503.22,-19.164,0.017975,19.174,0.11891,3.4203,-0.0020125,3.4203,-5.884e-4,1.9454,0.11754,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.056667,2353253,0,33.665,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.1155,284.82,95318,338.37,0.5,1.1868</datapoint>
- <datapoint>59.021,493.64,-19.155,0.017089,19.164,0.056464,2.4409,-0.0020125,2.4409,-8.245e-4,1.9723,0.053816,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.056631,2353737,0,33.66,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0501,284.88,95425,338.41,0.5,1.1869</datapoint>
- <datapoint>59.521,484.06,-19.147,0.017468,19.155,0.038027,1.4505,-0.0020125,1.4505,-0.0013874,1.9892,0.033777,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.056599,2354470,0,33.661,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.038,284.94,95535,338.44,0.5,1.1876</datapoint>
- <datapoint>60.021,474.49,-19.138,0.018044,19.147,0.064955,0.46375,-0.0020125,0.46376,-0.0043396,1.958,0.062398,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.056567,2355274,0,33.663,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.8678,285,95648,338.48,0.5,1.1878</datapoint>
- <datapoint>60.521,464.93,-19.129,0.017979,19.138,0.024565,-0.51732,-0.0020125,0.51732,-3.1377,1.9663,0.016739,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.056533,2355961,0,33.662,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9905,285.07,95760,338.52,0.5,1.1879</datapoint>
- <datapoint>61.021,455.36,-19.12,0.018123,19.129,0.02978,-1.4975,-0.0020125,1.4975,-3.1402,1.9545,0.02363,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.0565,2356696,0,33.663,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9204,285.13,95872,338.56,0.5,1.1881</datapoint>
- <datapoint>61.521,445.81,-19.11,0.019872,19.123,0.18636,-2.4979,-0.0020125,2.4979,-3.1408,2.0472,0.1853,NaN,NaN,NaN,NaN,3.4191,NaN,NaN,NaN,0.056477,2357824,0,33.675,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.3143,285.19,95984,338.6,0.5,1.1882</datapoint>
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</flightdata>
</simulation>
<?xml version='1.0' encoding='utf-8'?>
-<openrocket version="1.0" creator="OpenRocket 0.9.6">
+<openrocket version="1.0" creator="OpenRocket 0.9.7pre">
<rocket>
<name>Roll-stabilized rocket</name>
<comment>Canting the fins may increase the flight stability of a rocket.
Be cautios when flying rockets with marginal or neurtal static stability!!</comment>
<designer>Sampo Niskanen</designer>
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- <motorconfiguration configid="d33813f0-2563-41f7-8bb3-96eae598f567"/>
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+ <motorconfiguration configid="d33813f0-2563-41f7-8bb3-96eae598f567" default="true"/>
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<subcomponents>
<clusterrotation>0.0</clusterrotation>
<motormount>
<motor configid="e1dc7488-77c0-403a-b54f-c01db07aba2f">
+ <type>single</type>
<manufacturer>Estes</manufacturer>
<designation>D12</designation>
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<atmosphere model="isa"/>
<timestep>0.05</timestep>
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</databranch>
</flightdata>
</simulation>
<?xml version='1.0' encoding='utf-8'?>
-<openrocket version="1.0" creator="OpenRocket 0.9.6">
+<openrocket version="1.0" creator="OpenRocket 0.9.7pre">
<rocket>
<name>Three-staged rocket</name>
<comment>This example demonstrates a staged rocket design. Most operations, such as motor ignition, work correctly with the "Automatic" ignition setting, whereby the lowest stage ignites on launch and later stages at the deployment charge of the previous stage.
<clusterrotation>0.0</clusterrotation>
<motormount>
<motor configid="da326836-0959-4c94-bcd5-49dee07235a4">
+ <type>single</type>
<manufacturer>Estes</manufacturer>
<designation>A8</designation>
<diameter>0.018</diameter>
<delay>3.0</delay>
</motor>
<motor configid="05896b5a-71a7-48ac-b7ae-eadeb267975b">
+ <type>single</type>
<manufacturer>Estes</manufacturer>
<designation>C6</designation>
<diameter>0.018</diameter>
<delay>5.0</delay>
</motor>
<motor configid="b13e8ca2-f54d-4ca8-9b23-06c6c9eb237a">
+ <type>single</type>
<manufacturer>Estes</manufacturer>
<designation>C6</designation>
<diameter>0.018</diameter>
<clusterrotation>0.0</clusterrotation>
<motormount>
<motor configid="da326836-0959-4c94-bcd5-49dee07235a4">
+ <type>single</type>
<manufacturer>Estes</manufacturer>
<designation>B6</designation>
<diameter>0.018</diameter>
<delay>0.0</delay>
</motor>
<motor configid="05896b5a-71a7-48ac-b7ae-eadeb267975b">
+ <type>single</type>
<manufacturer>Estes</manufacturer>
<designation>B6</designation>
<diameter>0.018</diameter>
<delay>0.0</delay>
</motor>
<motor configid="b13e8ca2-f54d-4ca8-9b23-06c6c9eb237a">
+ <type>single</type>
<manufacturer>Estes</manufacturer>
<designation>C6</designation>
<diameter>0.018</diameter>
<clusterrotation>0.0</clusterrotation>
<motormount>
<motor configid="da326836-0959-4c94-bcd5-49dee07235a4">
+ <type>single</type>
<manufacturer>Estes</manufacturer>
<designation>B6</designation>
<diameter>0.018</diameter>
<delay>0.0</delay>
</motor>
<motor configid="05896b5a-71a7-48ac-b7ae-eadeb267975b">
+ <type>single</type>
<manufacturer>Estes</manufacturer>
<designation>B6</designation>
<diameter>0.018</diameter>
<delay>0.0</delay>
</motor>
<motor configid="b13e8ca2-f54d-4ca8-9b23-06c6c9eb237a">
+ <type>single</type>
<manufacturer>Estes</manufacturer>
<designation>C6</designation>
<diameter>0.018</diameter>
<atmosphere model="isa"/>
<timestep>0.05</timestep>
</conditions>
- <flightdata maxaltitude="217.21" maxvelocity="72.937" maxacceleration="221.28" maxmach="0.2145" timetoapogee="5.9808" flighttime="58.626" groundhitvelocity="3.9573">
+ <flightdata maxaltitude="208.2" maxvelocity="70.754" maxacceleration="112.12" maxmach="0.20807" timetoapogee="5.9595" flighttime="56.206" groundhitvelocity="3.9508">
<databranch name="Main" types="Time,Altitude,Vertical velocity,Vertical acceleration,Total velocity,Total acceleration,Position upwind,Position parallel to wind,Lateral distance,Lateral direction,Lateral velocity,Lateral acceleration,Angle of attack,Roll rate,Pitch rate,Yaw rate,Mass,CP location,CG location,Stability margin calibers,Mach number,Reynolds number,Thrust,Drag force,Drag coefficient,Axial drag coefficient,Friction drag coefficient,Pressure drag coefficient,Base drag coefficient,Normal force coefficient,Pitch moment coefficient,Yaw moment coefficient,Side force coefficient,Roll moment coefficient,Roll forcing coefficient,Roll damping coefficient,Pitch damping coefficient,Reference length,Reference area,Vertical orientation (zenith),Lateral orientation (azimuth),Wind velocity,Air temperature,Air pressure,Speed of sound,Simulation time step,Computation time">
<event time="0" type="launch"/>
<event time="0" type="ignition"/>
<event time="0.09" type="liftoff"/>
<event time="0.26" type="launchrod"/>
- <event time="0.86489" type="burnout"/>
- <event time="0.86489" type="ejectioncharge"/>
- <event time="0.86489" type="ignition"/>
- <event time="0.86489" type="stageseparation"/>
- <event time="1.7361" type="burnout"/>
- <event time="1.7361" type="ejectioncharge"/>
- <event time="1.7361" type="ignition"/>
- <event time="1.7361" type="stageseparation"/>
- <event time="2.5098" type="burnout"/>
- <event time="5.5152" type="ejectioncharge"/>
- <event time="5.5152" type="recoverydevicedeployment"/>
- <event time="6.0289" type="apogee"/>
- <event time="58.626" type="groundhit"/>
- <event time="58.626" type="simulationend"/>
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- <datapoint>0.2,0.44998,8.0043,68.949,8.3316,68.949,0,0,0,0,0,0,0.28122,0,0,0,0.12617,NaN,NaN,NaN,0.024477,315406,9.9921,0.053974,1.993,2.5862,0.9431,0.92986,0.12008,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,0.025,4.9087e-4,1.5708,0,2.3123,288.15,101320,340.39,0.01,0.54</datapoint>
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- <datapoint>11.52,195.2,-4.3248,-0.75521,4.0512,1.2639,40.852,0.0014063,40.852,3.4425e-5,2.0025,1.0135,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.011929,114655,0,0.55798,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0519,286.87,99016,339.61,0.3956,1.3804</datapoint>
- <datapoint>12.02,193.11,-4.0365,0.5766,4.3249,0.58023,39.858,0.0014063,39.858,3.5283e-5,1.9701,0.064779,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.012735,122418,0,0.63603,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9756,286.88,99036,339.62,0.5,1.3806</datapoint>
- <datapoint>12.52,191,-4.4142,-0.75532,4.0392,0.82378,38.914,0.0014063,38.914,3.6139e-5,1.8057,0.32879,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.011893,114349,0,0.55488,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.8237,286.89,99060,339.63,0.5,1.3807</datapoint>
- <datapoint>13.009,188.96,-3.9173,1.0153,4.4144,1.0215,38.044,0.0014063,38.044,3.6966e-5,1.7505,0.11289,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.012998,124993,0,0.66289,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.7597,286.91,99085,339.64,0.48946,1.3809</datapoint>
- <datapoint>13.398,187.34,-4.4158,-1.2846,3.9175,1.2884,37.357,0.0014063,37.357,3.7645e-5,1.7891,0.099493,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.011534,110941,0,0.52216,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.7962,286.92,99109,339.64,0.38807,1.3812</datapoint>
- <datapoint>13.813,185.6,-3.9826,1.0428,4.4225,1.2037,36.562,0.0014063,36.562,3.8464e-5,2.0388,0.60119,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.013021,125258,0,0.66556,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0336,286.93,99128,339.65,0.4154,1.3814</datapoint>
- <datapoint>14.29,183.59,-4.4539,-0.98841,3.9857,1.0485,35.63,0.0014063,35.63,3.947e-5,1.8719,0.34999,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.011735,112902,0,0.54067,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.8809,286.94,99148,339.66,0.47685,1.3815</datapoint>
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- <datapoint>16.409,174.67,-3.9595,1.2536,4.4595,1.2538,31.508,0.0014063,31.508,4.4634e-5,2.0638,0.018794,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.013128,126412,0,0.67744,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0638,287,99257,339.69,0.3988,1.3823</datapoint>
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- <datapoint>17.281,171.03,-3.9528,0.95969,4.4015,1.0806,29.6,0.0014063,29.6,4.7512e-5,2.0763,0.49677,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.012957,124802,0,0.66016,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.1035,287.03,99296,339.71,0.46269,1.3826</datapoint>
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- <datapoint>19.037,163.71,-3.9342,0.92733,4.3928,1.0187,26.17,0.0014063,26.17,5.3737e-5,2.0381,0.4217,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.01293,124623,0,0.65798,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0034,287.07,99381,339.74,0.49082,1.3832</datapoint>
- <datapoint>19.448,161.99,-4.4218,-1.1861,3.9361,1.2163,25.31,0.0014063,25.31,5.5564e-5,2.1488,0.26925,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.011586,111686,0,0.52841,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.1608,287.09,99405,339.74,0.41108,1.3834</datapoint>
- <datapoint>19.909,160.06,-3.9223,1.0824,4.4219,1.0833,24.323,0.0014063,24.323,5.7819e-5,2.1278,0.045384,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.013015,125485,0,0.66697,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.1304,287.1,99425,339.75,0.46154,1.3835</datapoint>
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- <datapoint>20.67,156.87,-4.0223,1.0996,4.4313,1.3898,22.724,0.0014063,22.724,6.1888e-5,1.8879,0.84985,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.013042,125787,0,0.67004,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.8497,287.12,99467,339.76,0.35977,1.3839</datapoint>
- <datapoint>21.17,154.77,-4.4089,-0.77325,4.0315,0.98669,21.856,0.0014063,21.856,6.4344e-5,1.5815,0.61289,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.011865,114453,0,0.55468,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.6153,287.13,99485,339.77,0.5,1.384</datapoint>
- <datapoint>21.647,152.78,-3.9179,1.028,4.4096,1.0468,21.078,0.0014063,21.078,6.6719e-5,1.6758,0.19758,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.012978,125208,0,0.66375,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.6618,287.14,99510,339.78,0.47764,1.3842</datapoint>
- <datapoint>22.041,151.14,-4.4104,-1.2501,3.9192,1.269,20.401,0.0014063,20.401,6.8933e-5,1.7619,0.21846,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.011534,111299,0,0.52441,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.7758,287.16,99533,339.79,0.394,1.3843</datapoint>
- <datapoint>22.47,149.34,-3.9603,1.0493,4.4152,1.1655,19.599,0.0014063,19.599,7.1756e-5,1.9796,0.50747,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.012994,125402,0,0.66566,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9679,287.17,99552,339.79,0.42899,1.3845</datapoint>
- <datapoint>22.897,147.55,-4.4079,-1.0481,3.9673,1.1707,18.706,0.0014063,18.706,7.5182e-5,2.2024,0.52164,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.011675,112696,0,0.53754,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.2152,287.18,99573,339.8,0.42709,1.3847</datapoint>
- <datapoint>23.298,145.87,-3.9872,1.0497,4.4164,1.2474,17.877,0.0014063,17.877,7.8667e-5,1.9323,0.67394,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.012997,125470,0,0.66624,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.929,287.19,99594,339.81,0.40083,1.3848</datapoint>
- <datapoint>23.798,143.76,-4.4579,-0.94136,3.9872,0.94192,16.915,0.0014063,16.915,8.3141e-5,1.916,0.032597,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.011734,113292,0,0.54313,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9176,287.2,99614,339.81,0.5,1.385</datapoint>
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- <datapoint>27.242,129.28,-4.4525,-1.0218,3.9671,1.0494,10.267,0.0014063,10.267,1.3697e-4,1.9755,0.23905,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.011672,112846,0,0.5384,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9694,287.3,99785,339.87,0.47648,1.3889</datapoint>
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- <datapoint>28.089,125.71,-4.4246,-0.8725,4.0026,1.0174,8.5203,0.0014063,8.5203,1.6506e-4,1.9219,0.52329,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.011776,113888,0,0.54828,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9453,287.32,99826,339.89,0.49145,1.3919</datapoint>
- <datapoint>28.519,123.91,-3.9357,1.1363,4.4257,1.1622,7.716,0.0014063,7.716,1.8226e-4,1.8169,0.24401,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.013021,125945,0,0.67043,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.8234,287.33,99851,339.89,0.43021,1.392</datapoint>
- <datapoint>28.929,122.2,-4.4026,-1.14,3.9407,1.2209,6.9353,0.0014063,6.9353,2.0278e-4,1.9959,0.4369,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.011594,112160,0,0.53164,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0151,287.34,99872,339.9,0.40954,1.3922</datapoint>
- <datapoint>29.414,120.19,-3.9034,1.0289,4.4027,1.0305,5.9601,0.0014063,5.9601,2.3596e-4,2.0239,0.057863,NaN,NaN,NaN,NaN,0.061193,NaN,NaN,NaN,0.012953,125324,0,0.6637,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0194,287.36,99892,339.91,0.48519,1.3923</datapoint>
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</databranch>
</flightdata>
</simulation>
<atmosphere model="isa"/>
<timestep>0.05</timestep>
</conditions>
- <flightdata maxaltitude="402.1" maxvelocity="108.23" maxacceleration="154.09" maxmach="0.3187" timetoapogee="8.8324" flighttime="105.64" groundhitvelocity="4.347">
+ <flightdata maxaltitude="397.36" maxvelocity="107.13" maxacceleration="154.63" maxmach="0.31543" timetoapogee="8.8588" flighttime="104.39" groundhitvelocity="4.3426">
<databranch name="Main" types="Time,Altitude,Vertical velocity,Vertical acceleration,Total velocity,Total acceleration,Position upwind,Position parallel to wind,Lateral distance,Lateral direction,Lateral velocity,Lateral acceleration,Angle of attack,Roll rate,Pitch rate,Yaw rate,Mass,CP location,CG location,Stability margin calibers,Mach number,Reynolds number,Thrust,Drag force,Drag coefficient,Axial drag coefficient,Friction drag coefficient,Pressure drag coefficient,Base drag coefficient,Normal force coefficient,Pitch moment coefficient,Yaw moment coefficient,Side force coefficient,Roll moment coefficient,Roll forcing coefficient,Roll damping coefficient,Pitch damping coefficient,Reference length,Reference area,Vertical orientation (zenith),Lateral orientation (azimuth),Wind velocity,Air temperature,Air pressure,Speed of sound,Simulation time step,Computation time">
<event time="0" type="launch"/>
<event time="0" type="ignition"/>
<event time="0.09" type="liftoff"/>
<event time="0.27" type="launchrod"/>
- <event time="0.85988" type="burnout"/>
- <event time="0.85988" type="ejectioncharge"/>
- <event time="0.85988" type="ignition"/>
- <event time="0.85988" type="stageseparation"/>
- <event time="1.7215" type="burnout"/>
- <event time="1.7215" type="ejectioncharge"/>
- <event time="1.7215" type="ignition"/>
- <event time="1.7215" type="stageseparation"/>
- <event time="3.6084" type="burnout"/>
- <event time="8.6208" type="ejectioncharge"/>
- <event time="8.6208" type="recoverydevicedeployment"/>
- <event time="8.8629" type="apogee"/>
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- <datapoint>110.57,108.01,-4.3776,-1.1537,3.9105,1.2236,19.691,0.0075188,19.691,3.8184e-4,2.1198,0.40761,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.011503,111420,0,0.52422,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.137,287.44,100038,339.96,0.40864,1.1488</datapoint>
- <datapoint>110.95,106.44,-3.9714,1.0809,4.3887,1.3307,18.84,0.0075188,18.84,3.9909e-4,2.4114,0.77609,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.012909,125062,0,0.66037,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.4315,287.45,100058,339.96,0.37574,1.2037</datapoint>
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- <datapoint>111.87,102.59,-3.904,1.1843,4.4031,1.1865,16.73,0.0075188,16.73,4.4941e-4,2.2227,0.072928,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.012951,125510,0,0.66497,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.2243,287.47,100101,339.98,0.42139,1.204</datapoint>
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- <datapoint>112.73,99.018,-3.8904,1.1199,4.3895,1.1221,14.897,0.0075188,14.897,5.0472e-4,2.0715,0.070479,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.012911,125155,0,0.66107,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0746,287.49,100142,339.99,0.44558,1.2043</datapoint>
- <datapoint>113.12,97.406,-4.3648,-1.2146,3.8947,1.2802,14.119,0.0075188,14.119,5.3254e-4,1.9135,0.40456,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.011455,111062,0,0.52053,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.8885,287.51,100164,340,0.39055,1.2044</datapoint>
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- <datapoint>113.99,93.86,-4.3478,-1.314,3.8713,1.3677,12.412,0.0075188,12.412,6.0577e-4,2.1035,0.37953,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.011386,110425,0,0.51446,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.1374,287.53,100207,340.01,0.36558,1.2047</datapoint>
- <datapoint>114.49,91.801,-3.8862,0.92325,4.349,0.95694,11.329,0.0075188,11.329,6.6369e-4,2.2294,0.25168,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.01279,124065,0,0.64935,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.2054,287.54,100224,340.02,0.5,1.2048</datapoint>
- <datapoint>114.84,90.344,-4.315,-1.2068,3.8999,1.4071,10.582,0.0075188,10.582,7.1051e-4,1.9722,0.72362,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.011469,111271,0,0.52226,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9028,287.55,100248,340.03,0.35534,1.2049</datapoint>
- <datapoint>115.34,88.283,-3.9279,0.77417,4.3198,0.92171,9.5335,0.0075188,9.5335,7.8866e-4,2.2223,0.50021,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.012704,123266,0,0.64088,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.176,287.56,100265,340.03,0.5,1.2051</datapoint>
- <datapoint>115.82,86.293,-4.4276,-1.0488,3.9279,1.0494,8.4707,0.0075188,8.4707,8.8762e-4,2.2388,0.034478,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.011551,112101,0,0.52998,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.2378,287.58,100290,340.04,0.47648,1.2052</datapoint>
- <datapoint>116.19,84.721,-3.9286,1.3265,4.4278,1.3292,7.6346,0.0075188,7.6346,9.8482e-4,2.2068,0.085101,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.013021,126385,0,0.67357,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.2049,287.59,100313,340.05,0.37615,1.2053</datapoint>
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- <datapoint>117.02,81.249,-3.9563,1.3342,4.4305,1.419,5.8611,0.0075188,5.8611,0.0012828,1.9889,0.48343,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.013029,126499,0,0.67464,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9673,287.61,100355,340.06,0.35235,1.2056</datapoint>
- <datapoint>117.52,79.156,-4.4142,-0.91572,3.9563,0.91578,4.8654,0.0075188,4.8654,0.0015453,1.9939,0.0099974,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.011634,112972,0,0.53802,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9933,287.62,100372,340.07,0.5,1.2057</datapoint>
- <datapoint>117.88,77.682,-3.9626,1.2827,4.4208,1.4203,4.1257,0.0075188,4.1257,0.0018224,2.2086,0.60999,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.012999,126256,0,0.67191,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.2364,287.64,100397,340.08,0.35203,1.2059</datapoint>
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- <datapoint>118.79,73.911,-3.9102,0.93294,4.3493,1.0754,2.2785,0.0075188,2.2785,0.0032999,2.1339,0.53491,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.012789,124246,0,0.65056,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.1014,287.66,100436,340.09,0.46494,1.2061</datapoint>
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+ <datapoint>134.35,14.533,-4.3887,-1.1622,3.8893,1.1635,-37.987,-0.0018149,37.987,-3.1415,1.7392,0.05519,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.011428,111608,0,0.52313,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.7381,288.04,101134,340.32,0.42975,1.5446</datapoint>
+ <datapoint>134.72,12.969,-3.9308,1.2179,4.3938,1.3299,-38.679,-0.0018149,38.679,-3.1415,1.94,0.53412,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.01291,126102,0,0.66776,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9516,288.06,101155,340.33,0.37598,1.5447</datapoint>
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+ <datapoint>135.59,9.3435,-3.9176,1.3547,4.4176,1.3548,-40.364,-0.0018149,40.364,-3.1415,1.9397,0.0046217,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.01298,126820,0,0.67525,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9398,288.08,101197,340.35,0.36907,1.552</datapoint>
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+ <datapoint>136.44,5.8178,-3.9178,1.2603,4.3995,1.3151,-42.069,-0.0018149,42.069,-3.1415,1.9393,0.37553,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.012926,126332,0,0.66993,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.933,288.1,101238,340.36,0.38021,1.5522</datapoint>
+ <datapoint>136.9,3.9162,-4.3839,-1.0174,3.9217,1.0914,-42.916,-0.0018149,42.916,-3.1416,1.7583,0.39502,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.011522,112627,0,0.53241,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.7634,288.11,101257,340.37,0.45812,1.5524</datapoint>
+ <datapoint>137.32,2.1819,-3.8839,1.1918,4.3839,1.1918,-43.654,-0.0018149,43.654,-3.1416,1.7575,0.001865,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.01288,125917,0,0.6654,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.7575,288.12,101279,340.37,0.41954,1.5525</datapoint>
+ <datapoint>137.7,0.59091,-4.3315,-1.1558,3.8924,1.2909,-44.377,-0.0018149,44.377,-3.1416,1.9802,0.57502,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.011436,111816,0,0.52466,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,2.0154,288.14,101299,340.38,0.38732,1.5526</datapoint>
+ <datapoint>138.2,-1.4581,-3.8646,0.93386,4.3316,0.93465,-45.372,-0.0018149,45.372,-3.1416,1.9995,0.03848,NaN,NaN,NaN,NaN,0.060443,NaN,NaN,NaN,0.012725,124446,0,0.64982,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,NaN,1.9957,288.15,101318,340.39,0.5,1.5527</datapoint>
</databranch>
</flightdata>
</simulation>
+++ /dev/null
-Rocket motor simulation data downloaded from ThrustCurve.org.\r
-This ZIP file contains 526 simulator data files.\r
-For more info, please see http://www.thrustcurve.org/\r
-\r
-AMW_I195.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: WW-38-390\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: John DeMar\r
-\r
-AMW_I220.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: SK-38-390\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: John DeMar\r
-\r
-AMW_I271.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: BB-38-390\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Greg Gardner\r
-\r
-AMW_I285.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: GG-38-390\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Greg Gardner\r
-\r
-AMW_I315.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: SK-38-640\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Koen Loeven\r
-\r
-AMW_I325.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: WW-38-640\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: John DeMar\r
-\r
-AMW_I375.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: GG-38-640\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Robert DeHate\r
-\r
-AMW_J357.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: WT-54-1050\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Carl Tulanko\r
-\r
-AMW_J365.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: SK-54-1400\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Robert DeHate\r
-\r
-AMW_J370.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: GG-54-1050\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_J400.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: RR-54-1050\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_J440.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: BB-38-640\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Robert DeHate\r
-\r
-AMW_J450.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: ST-54-1050\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Conway Stevens\r
-\r
-AMW_J450_1.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: ST-54-1050\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Carl Tulanko\r
-\r
-AMW_J480.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: BB-54-1050\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_J500.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: J500ST\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_K1000.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: SK-54-2550\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_K1075.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: GG-54-2550\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_K365.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: RR-75-1700\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_K450.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: BB-75-1700\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_K470.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: ST-75-1700\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_K475.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: WT-54-1400\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_K530.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: GG-54-1400\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_K555.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: SK-54-1750\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Koen Loeven\r
-\r
-AMW_K560.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: RR-54-1400\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_K570.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: WT-54-1750\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Carl Tulanko\r
-\r
-AMW_K600.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: WT-75-2500\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Conway Stevens\r
-\r
-AMW_K600_1.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: WT-75-2500\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Carl Tulanko\r
-\r
-AMW_K605.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: RR-75-2500\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_K650.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: RR-54-1750\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Koen Loeven\r
-\r
-AMW_K670.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: GG-54-1750\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Conway Stevens\r
-\r
-AMW_K670_1.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: GG-54-1750\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Carl Tulanko\r
-\r
-AMW_K700.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: BB-54-1400\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_K800.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: BB-54-1750\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Koen Loeven\r
-\r
-AMW_K950.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: ST-54-1750\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Conway Stevens\r
-\r
-AMW_K950_1.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: ST-54-1750\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Carl Tulanko\r
-\r
-AMW_K975.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: WT-54-2550\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Carl Tulanko\r
-\r
-AMW_L1060.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: GG-75-3500\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Conway Stevens\r
-\r
-AMW_L1060_1.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: GG-75-3500\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Carl Tulanko\r
-\r
-AMW_L1080.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: BB-75-3500\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_L1100.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: RR-54-2550\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_L1111.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: ST-75-3500\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_L1300.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: BB-54-2550\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_L1400.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: SK-75-6000\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: John DeMar\r
-\r
-AMW_L666.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: SK-75-3500\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Joel Rogers\r
-\r
-AMW_L700.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: BB-75-2500\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_L777.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: WT-75-3500\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Conway Stevens\r
-\r
-AMW_L777_1.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: WT-75-3500\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Carl Tulanko\r
-\r
-AMW_L900.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: RR-75-3500\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_M1350.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: WT-75-6000\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Carl Tulanko\r
-\r
-AMW_M1480.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: RR-75-6000\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_M1730.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: SK-98-11000\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Joel Rogers\r
-\r
-AMW_M1850.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: GG-75-6000\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Conway Stevens\r
-\r
-AMW_M1850_1.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: GG-75-6000\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Carl Tulanko\r
-\r
-AMW_M1900.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: BB-75-6000\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_M2500.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: GG-75-7600\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Carl Tulanko\r
-\r
-AMW_M3000.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: ST-75-7600\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Conway Stevens\r
-\r
-AMW_N2020.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: WT-98-11000\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Joel Rogers\r
-\r
-AMW_N2600.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: GG-98-11000\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_N2700.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: BB-98-11000\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AMW_N2800.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: WW-98-17500\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: John DeMar\r
-\r
-AMW_N4000.eng\r
- Manufacturer: Animal Motor Works\r
- Designation: BB-98-17500\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Robert DeHate\r
-\r
-AeroTech_D13.eng\r
- Manufacturer: AeroTech\r
- Designation: D13\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Christopher Kobel\r
-\r
-AeroTech_D15.eng\r
- Manufacturer: AeroTech\r
- Designation: D15\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Christopher Kobel\r
-\r
-AeroTech_D21.eng\r
- Manufacturer: AeroTech\r
- Designation: D21\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Christopher Kobel\r
-\r
-AeroTech_D24.eng\r
- Manufacturer: AeroTech\r
- Designation: D24\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Stan Hemphill\r
-\r
-AeroTech_D7.eng\r
- Manufacturer: AeroTech\r
- Designation: D7\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AeroTech_D9.eng\r
- Manufacturer: AeroTech\r
- Designation: D9\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Christopher Kobel\r
-\r
-AeroTech_E11.eng\r
- Manufacturer: AeroTech\r
- Designation: E11J\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AeroTech_E12.eng\r
- Manufacturer: AeroTech\r
- Designation: E12J\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AeroTech_E15.eng\r
- Manufacturer: AeroTech\r
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- Contributor: Greg Gardner\r
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-AeroTech_I115.eng\r
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-AeroTech_I132.eng\r
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- Data Source: cert\r
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- Data Source: cert\r
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- Data Source: cert\r
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-AeroTech_I195.eng\r
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- Data Source: cert\r
- Contributor: John Coker\r
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-AeroTech_I195_1.eng\r
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- Data Source: cert\r
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-AeroTech_I200.eng\r
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- Data Format: RASP\r
- Data Source: cert\r
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-AeroTech_I211.eng\r
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- Data Source: cert\r
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-AeroTech_I215.eng\r
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- Data Source: cert\r
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-AeroTech_I218.eng\r
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- Data Format: RASP\r
- Data Source: cert\r
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-AeroTech_I225.eng\r
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-\r
-AeroTech_I229.eng\r
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- Data Format: RASP\r
- Data Source: cert\r
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-AeroTech_I245.eng\r
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-\r
-AeroTech_I284.eng\r
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- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_I284_1.eng\r
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- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_I285.eng\r
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- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_I300.eng\r
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- Designation: I300T\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AeroTech_I305.eng\r
- Manufacturer: AeroTech\r
- Designation: I305FJ\r
- Data Format: RASP\r
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- Contributor: Christopher Kobel\r
-\r
-AeroTech_I357.eng\r
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- Data Format: RASP\r
- Data Source: cert\r
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-AeroTech_I364.eng\r
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-\r
-AeroTech_I366.eng\r
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- Data Format: RASP\r
- Data Source: cert\r
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-\r
-AeroTech_I435.eng\r
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- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_I435_1.eng\r
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- Data Format: RASP\r
- Data Source: cert\r
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-\r
-AeroTech_I599.eng\r
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- Data Format: RASP\r
- Data Source: cert\r
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-\r
-AeroTech_I600.eng\r
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- Data Format: RASP\r
- Data Source: user\r
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-\r
-AeroTech_I65.eng\r
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- Data Format: RASP\r
- Data Source: cert\r
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-\r
-AeroTech_J125.eng\r
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- Data Format: RASP\r
- Data Source: cert\r
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-\r
-AeroTech_J1299.eng\r
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- Data Format: RASP\r
- Data Source: user\r
- Contributor: Greg Gardner\r
-\r
-AeroTech_J135.eng\r
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- Data Format: RASP\r
- Data Source: cert\r
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-\r
-AeroTech_J145.eng\r
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- Data Format: RASP\r
- Data Source: cert\r
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-\r
-AeroTech_J180.eng\r
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- Data Format: RASP\r
- Data Source: cert\r
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-\r
-AeroTech_J1999.eng\r
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- Designation: J1999N-P\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Greg Gardner\r
-\r
-AeroTech_J210.eng\r
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- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AeroTech_J250.eng\r
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- Designation: J250FJ\r
- Data Format: RASP\r
- Data Source: cert\r
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-\r
-AeroTech_J260.eng\r
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- Designation: J260HW 3-jet EFX\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AeroTech_J275.eng\r
- Manufacturer: AeroTech\r
- Designation: J275W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_J315.eng\r
- Manufacturer: AeroTech\r
- Designation: J315R\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_J350.eng\r
- Manufacturer: AeroTech\r
- Designation: J350W-L\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AeroTech_J350_1.eng\r
- Manufacturer: AeroTech\r
- Designation: J350W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_J390.eng\r
- Manufacturer: AeroTech\r
- Designation: J390-turbo\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AeroTech_J415.eng\r
- Manufacturer: AeroTech\r
- Designation: J415W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_J420.eng\r
- Manufacturer: AeroTech\r
- Designation: J420R\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_J460.eng\r
- Manufacturer: AeroTech\r
- Designation: J460T\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_J500.eng\r
- Manufacturer: AeroTech\r
- Designation: J500G\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Jim Yehle\r
-\r
-AeroTech_J540.eng\r
- Manufacturer: AeroTech\r
- Designation: J540R\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_J570.eng\r
- Manufacturer: AeroTech\r
- Designation: J570W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_J575.eng\r
- Manufacturer: AeroTech\r
- Designation: J575FJ\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Simon Crafts\r
-\r
-AeroTech_J800.eng\r
- Manufacturer: AeroTech\r
- Designation: J800T-PS\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_J825.eng\r
- Manufacturer: AeroTech\r
- Designation: J825R\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Greg Gardner\r
-\r
-AeroTech_J90.eng\r
- Manufacturer: AeroTech\r
- Designation: J90W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_K1050.eng\r
- Manufacturer: AeroTech\r
- Designation: K1050W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_K1100.eng\r
- Manufacturer: AeroTech\r
- Designation: K1100T\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_K1275.eng\r
- Manufacturer: AeroTech\r
- Designation: K1275\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_K1499.eng\r
- Manufacturer: AeroTech\r
- Designation: K1499N-P\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Jim Yehle\r
-\r
-AeroTech_K185.eng\r
- Manufacturer: AeroTech\r
- Designation: K185W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_K1999.eng\r
- Manufacturer: AeroTech\r
- Designation: K1999N-P\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Christopher Kobel\r
-\r
-AeroTech_K250.eng\r
- Manufacturer: AeroTech\r
- Designation: K250W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_K270.eng\r
- Manufacturer: AeroTech\r
- Designation: K270W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Mark Koelsch\r
-\r
-AeroTech_K458.eng\r
- Manufacturer: AeroTech\r
- Designation: K458W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_K485.eng\r
- Manufacturer: AeroTech\r
- Designation: K485H (3 jet)\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_K550.eng\r
- Manufacturer: AeroTech\r
- Designation: K550W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_K560.eng\r
- Manufacturer: AeroTech\r
- Designation: K560W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_K650.eng\r
- Manufacturer: AeroTech\r
- Designation: K650T\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_K680.eng\r
- Manufacturer: AeroTech\r
- Designation: K680R\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AeroTech_K695.eng\r
- Manufacturer: AeroTech\r
- Designation: K695R\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_K700.eng\r
- Manufacturer: AeroTech\r
- Designation: K700W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_K780.eng\r
- Manufacturer: AeroTech\r
- Designation: K780R\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_K828.eng\r
- Manufacturer: AeroTech\r
- Designation: K828FJ\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Mark Koelsch\r
-\r
-AeroTech_L1120.eng\r
- Manufacturer: AeroTech\r
- Designation: L1120W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_L1150.eng\r
- Manufacturer: AeroTech\r
- Designation: L1150R\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_L1300.eng\r
- Manufacturer: AeroTech\r
- Designation: L1300R\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AeroTech_L1420.eng\r
- Manufacturer: AeroTech\r
- Designation: L1420R\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AeroTech_L1500.eng\r
- Manufacturer: AeroTech\r
- Designation: L1500T\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_L850.eng\r
- Manufacturer: AeroTech\r
- Designation: L850W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_L952.eng\r
- Manufacturer: AeroTech\r
- Designation: L952W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_M1297.eng\r
- Manufacturer: AeroTech\r
- Designation: M1297W\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Greg Gardner\r
-\r
-AeroTech_M1315.eng\r
- Manufacturer: AeroTech\r
- Designation: M1315W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_M1419.eng\r
- Manufacturer: AeroTech\r
- Designation: M1419W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_M1550.eng\r
- Manufacturer: AeroTech\r
- Designation: M1550R\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_M1600.eng\r
- Manufacturer: AeroTech\r
- Designation: M1600R\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_M1850.eng\r
- Manufacturer: AeroTech\r
- Designation: M1850W-PS\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Greg Gardner\r
-\r
-AeroTech_M1939.eng\r
- Manufacturer: AeroTech\r
- Designation: M1939W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_M2000.eng\r
- Manufacturer: AeroTech\r
- Designation: M2000R\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_M2400.eng\r
- Manufacturer: AeroTech\r
- Designation: M2400T\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_M2500.eng\r
- Manufacturer: AeroTech\r
- Designation: M2500T\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_M650.eng\r
- Manufacturer: AeroTech\r
- Designation: M650W\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Greg Gardner\r
-\r
-AeroTech_M750.eng\r
- Manufacturer: AeroTech\r
- Designation: M750W\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Greg Gardner\r
-\r
-AeroTech_M845.eng\r
- Manufacturer: AeroTech\r
- Designation: M845\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-AeroTech_N2000.eng\r
- Manufacturer: AeroTech\r
- Designation: N2000W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-AeroTech_N4800.eng\r
- Manufacturer: AeroTech\r
- Designation: N4800T\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Apogee_1/2A2.eng\r
- Manufacturer: Apogee Components\r
- Designation: 1/2A2\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Apogee_1/4A2.eng\r
- Manufacturer: Apogee Components\r
- Designation: 1/4A2\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Apogee_A2.eng\r
- Manufacturer: Apogee Components\r
- Designation: A2\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Apogee_B2.eng\r
- Manufacturer: Apogee Components\r
- Designation: B2\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Apogee_B7.eng\r
- Manufacturer: Apogee Components\r
- Designation: B7\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Apogee_C10.eng\r
- Manufacturer: Apogee Components\r
- Designation: C10\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Apogee_C4.eng\r
- Manufacturer: Apogee Components\r
- Designation: C4\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Apogee_C6.eng\r
- Manufacturer: Apogee Components\r
- Designation: C6\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Apogee_D10.eng\r
- Manufacturer: Apogee Components\r
- Designation: D10\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Apogee_D3.eng\r
- Manufacturer: Apogee Components\r
- Designation: D3\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Apogee_E6.eng\r
- Manufacturer: Apogee Components\r
- Designation: E6\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Apogee_F10.eng\r
- Manufacturer: Apogee Components\r
- Designation: F10\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Cesaroni_G60.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 134 G60-14A\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Cesaroni_G69.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 121 G69-14A\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Pete Carr\r
-\r
-Cesaroni_G69_1.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 121 G69-14A\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_G79.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 129 G79SS-13A\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: Pete Carr\r
-\r
-Cesaroni_G79_1.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 129 G79SS-13A\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_H120.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 261 H120-14A\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Len Bryan\r
-\r
-Cesaroni_H143.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 247 H143SS-13A\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_H153.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: H153\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_H565.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: H565\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Cesaroni_I170.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 382 I170-14A\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Cesaroni_I205.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: I205\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_I212.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 364 I212SS-14A\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_I240.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: I240\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Cesaroni_I285.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: I285\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_I287.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 486 I287SS-15A\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_I350.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 601 I350SS-16A\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_I360.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: I360\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Cesaroni_I540.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 634I540WT\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Cesaroni_J210.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 836 J210-16A\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_J280.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: J280SS\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_J285.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 648 J285-15A\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_J295.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 1195 J295-15A\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_J300.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: J300\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Cesaroni_J330.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 765 J330-16A\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_J360.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: J360\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Cesaroni_J380.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 1043 J380SS-16A\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_J400.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: J400SS\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_J410.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 774 J410-16A\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Len Bryan\r
-\r
-Cesaroni_K445.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 1635 K445-A\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_K510.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 2486 K510-P-U\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Len Lekx\r
-\r
-Cesaroni_K510_1.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 2486 K510-P-U\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_K530.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 1412 K530SS-16A\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_K570.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 2060 K570-A\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_K575.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 2493 K575-P\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Cesaroni_K650.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 1750 K650SS-16A\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_K660.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 2437 K660-17A\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_L1090.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 4815 L1090-P\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Cesaroni_L1115.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 5015 L1115-P-U\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Len Lekx\r
-\r
-Cesaroni_L1115_1.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 5015 L1115-P-U\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_L610.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 4842 L610-P\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Cesaroni_L730.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 2765 L730-P\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_L800.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 3757 L800-P-U\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Len Lekx\r
-\r
-Cesaroni_L800_1.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 3757 L800-P-U\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_L890.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 3762 L890-P\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Cesaroni_M1060.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 7441 M1060-P\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Cesaroni_M1400.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 6251 M1400-P-U\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Len Lekx\r
-\r
-Cesaroni_M1400_1.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 6251 M1400-P-U\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_M1450.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 9955 M1450-P\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Cesaroni_M2505.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 7450 M2505-P\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_M520.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 7400 M520-P\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_M795.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 10133 M795-P\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Cesaroni_N1100.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 14005 N1100-P\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Cesaroni_N2500.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 13766 N2500-P\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Casey Hatch\r
-\r
-Cesaroni_O5100.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 29990 O5100-P\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Cesaroni_O5800.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 30605 O5800-P\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Len Bryan\r
-\r
-Cesaroni_O8000.eng\r
- Manufacturer: Cesaroni Technology Inc.\r
- Designation: 40960 O8000-P\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Len Bryan\r
-\r
-Contrail_G100.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: G100-PVC\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_G123.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: G123-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_G130.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: G130-PVC\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_G234.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: G234-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_G300.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: G300-PVC\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_H121.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: H121-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_H141.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: H141-PVC\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_H211.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: H211-PVC\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_H222.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: H222-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_H246.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: H246-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_H277.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: H277-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_H300.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: H300-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_H303.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: H303-PVC\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_H340.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: H340-SP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_I155.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: I155-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_I210.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: I210-PVC\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_I221.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: I221-PVC\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_I290.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: I290-SP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_I307.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: I307-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_I333.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: I333-PVC\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_I400.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: I400-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_I500.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: I500-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_I727.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: I727-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_I747.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: I747-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_J150.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: J150-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_J222.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: J222-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_J234.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: J234-BG\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_J242.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: J242-PVC\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_J245.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: J245-BG\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_J246.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: J246-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_J272.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: J272-SP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_J292.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: J292-SP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_J333.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: J333-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_J345.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: J345-PVC\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_J355.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: J355-BG\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_J358.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: J358-BG\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_J416.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: J416-SP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_J555.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: J555-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_J642.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: J642-BG\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_J800.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: J800-HP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_K234.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: K234-BG\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_K265.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: K265-SP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_K300.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: K300-BS\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_K321.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: K321-BG\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_K404.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: K404-SP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_K456.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: K456-BG\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_K630.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: K630-SP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_K678.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: K678-BG\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_K707.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: K707-BG\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_K777.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: K777-SP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_L1222.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: L1222-SM\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_L2525.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: L2525-GF\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_L369.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: L369-SP\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_L800.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: L800-BG\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_M1575.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: M1575-BG\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_M2700.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: M2700-BS\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_M2800.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: M2800-BG\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_M711.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: M711-BS\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Contrail_O6300.eng\r
- Manufacturer: Contrail Rockets LLC\r
- Designation: O6300-BS\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Ellis_G20.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: G20\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Ellis_G35.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: G35\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Ellis_G37.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: G37\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Ellis_H275.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: H275\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Ellis_H48.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: H48\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Ellis_H50.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: H50\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Ellis_I130.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: I130\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Ellis_I134.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: I134\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Ellis_I150.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: I150\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Ellis_I160.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: I160\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Ellis_I230.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: I230\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Ellis_I69.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: I69\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Ellis_J110.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: J110\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Ellis_J148.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: J148\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Ellis_J228.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: J228\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Ellis_J270.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: J270\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Ellis_J330.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: J330\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Ellis_K475.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: K475\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Ellis_L330.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: L330\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Ellis_L600.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: L600\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Ellis_M1000.eng\r
- Manufacturer: Ellis Mountain Rocket Works\r
- Designation: M1000\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Estes_1/2A3.eng\r
- Manufacturer: Estes Industries\r
- Designation: 1/2A3\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Estes_1/2A6.eng\r
- Manufacturer: Estes Industries\r
- Designation: 1/2A6\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Estes_1/4A3.eng\r
- Manufacturer: Estes Industries\r
- Designation: 1/4A3\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Estes_A10.eng\r
- Manufacturer: Estes Industries\r
- Designation: A10\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Estes_A3.eng\r
- Manufacturer: Estes Industries\r
- Designation: A3\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Estes_A8.eng\r
- Manufacturer: Estes Industries\r
- Designation: A8\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Estes_B4.eng\r
- Manufacturer: Estes Industries\r
- Designation: B4\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Estes_B6.eng\r
- Manufacturer: Estes Industries\r
- Designation: B6\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Mark Koelsch\r
-\r
-Estes_C11.eng\r
- Manufacturer: Estes Industries\r
- Designation: C11\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Estes_C5.eng\r
- Manufacturer: Estes Industries\r
- Designation: C5\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Estes_C6.eng\r
- Manufacturer: Estes Industries\r
- Designation: C6\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Estes_D11.eng\r
- Manufacturer: Estes Industries\r
- Designation: D11\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Estes_D12.eng\r
- Manufacturer: Estes Industries\r
- Designation: D12\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Estes_E9.eng\r
- Manufacturer: Estes Industries\r
- Designation: E9\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Mark Koelsch\r
-\r
-GR_K555.eng\r
- Manufacturer: Gorilla Rocket Motors, Inc.\r
- Designation: K555GT\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Mark Koelsch\r
-\r
-Hypertek_I130.eng\r
- Manufacturer: Hypertek\r
- Designation: 300CC098J - I130\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Hypertek_I136.eng\r
- Manufacturer: Hypertek\r
- Designation: 300CC098J2 - I136\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Hypertek_I145.eng\r
- Manufacturer: Hypertek\r
- Designation: 300CC098JFX - I145FX\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Hypertek_I205.eng\r
- Manufacturer: Hypertek\r
- Designation: 300CC125J - I205\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Hypertek_I222.eng\r
- Manufacturer: Hypertek\r
- Designation: 300CC125J2 - I222\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Hypertek_I225.eng\r
- Manufacturer: Hypertek\r
- Designation: 300CC125JFX - I225FX\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Hypertek_I260.eng\r
- Manufacturer: Hypertek\r
- Designation: 440CC172J - I260\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Hypertek_I310.eng\r
- Manufacturer: Hypertek\r
- Designation: 440CC172J - I310\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_J115.eng\r
- Manufacturer: Hypertek\r
- Designation: 440CC076J - J115\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_J120.eng\r
- Manufacturer: Hypertek\r
- Designation: 440CC076JFX - J120FX\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_J150.eng\r
- Manufacturer: Hypertek\r
- Designation: 440CC086J - J150\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_J170.eng\r
- Manufacturer: Hypertek\r
- Designation: 440CC098J - J170\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_J190.eng\r
- Manufacturer: Hypertek\r
- Designation: 440CC098JFX - J190FX\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_J220.eng\r
- Manufacturer: Hypertek\r
- Designation: 440CC110J - J220\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_J250.eng\r
- Manufacturer: Hypertek\r
- Designation: 440CC125J - J250\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_J250_1.eng\r
- Manufacturer: Hypertek\r
- Designation: 440CC125J - J250\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_J270.eng\r
- Manufacturer: Hypertek\r
- Designation: 440CC125JFX - J270FX\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_J295.eng\r
- Manufacturer: Hypertek\r
- Designation: 440CC172JFX - J295FX\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Hypertek_J317.eng\r
- Manufacturer: Hypertek\r
- Designation: 835CC172J - J317\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_J330.eng\r
- Manufacturer: Hypertek\r
- Designation: 835CC172JFX - J330FX\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_J330_1.eng\r
- Manufacturer: Hypertek\r
- Designation: 835CC172JFX - J330FX\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_K240.eng\r
- Manufacturer: Hypertek\r
- Designation: 835CC125J - K240\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L200.eng\r
- Manufacturer: Hypertek\r
- Designation: 1685CC098L - L200\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L225.eng\r
- Manufacturer: Hypertek\r
- Designation: 1685CC098LFX - L225FX\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L350.eng\r
- Manufacturer: Hypertek\r
- Designation: 1685CC125L - L350\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L355.eng\r
- Manufacturer: Hypertek\r
- Designation: 1685CC125LFX - L355FX\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L475.eng\r
- Manufacturer: Hypertek\r
- Designation: 1685CC172L - L475\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L535.eng\r
- Manufacturer: Hypertek\r
- Designation: 1685CC172LFX - L535FX\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L540.eng\r
- Manufacturer: Hypertek\r
- Designation: 2800CC172L - L540\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L540_1.eng\r
- Manufacturer: Hypertek\r
- Designation: 2800CC172L - L540\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L550.eng\r
- Manufacturer: Hypertek\r
- Designation: 1685CCRGL - L550\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L570.eng\r
- Manufacturer: Hypertek\r
- Designation: 2800CC172LFX - L570FX\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L570_1.eng\r
- Manufacturer: Hypertek\r
- Designation: 2800CC172LFX - L570FX\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L575.eng\r
- Manufacturer: Hypertek\r
- Designation: 2800CCRGL - L575\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L575_1.eng\r
- Manufacturer: Hypertek\r
- Designation: 2800CCRGL - L575\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L610.eng\r
- Manufacturer: Hypertek\r
- Designation: 1685CCRGLFX - L610FX\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L625.eng\r
- Manufacturer: Hypertek\r
- Designation: 2800CCRGLFX - L625FX\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L625_1.eng\r
- Manufacturer: Hypertek\r
- Designation: 2800CCRGLFX - L625FX\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_L740.eng\r
- Manufacturer: Hypertek\r
- Designation: 2800CC200MFX - L740FX\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Hypertek_L970.eng\r
- Manufacturer: Hypertek\r
- Designation: 2800CC300M - L970\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Hypertek_M1000.eng\r
- Manufacturer: Hypertek\r
- Designation: 4630CCRGM - M1000\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_M1000_1.eng\r
- Manufacturer: Hypertek\r
- Designation: 4630CCRGM - M1000\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_M1001.eng\r
- Manufacturer: Hypertek\r
- Designation: 5478CCRGM - M1001\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Hypertek_M1010.eng\r
- Manufacturer: Hypertek\r
- Designation: 4630CCRGMFX - M1010FX\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_M1010_1.eng\r
- Manufacturer: Hypertek\r
- Designation: 4630CCRGMFX - M1010FX\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-Hypertek_M1015.eng\r
- Manufacturer: Hypertek\r
- Designation: 3500CCRGMFX - M1015FX\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Hypertek_M1040.eng\r
- Manufacturer: Hypertek\r
- Designation: 4630CCRGMFX - M1040FX\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Hypertek_M740.eng\r
- Manufacturer: Hypertek\r
- Designation: 2800CC200M - M740\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Hypertek_M956.eng\r
- Manufacturer: Hypertek\r
- Designation: 3500CCRGM - M956\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Hypertek_M960.eng\r
- Manufacturer: Hypertek\r
- Designation: 2800CC300MFX - M960FX\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-KBA_I170.eng\r
- Manufacturer: Kosdon by AeroTech\r
- Designation: I170S\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-KBA_I280.eng\r
- Manufacturer: Kosdon by AeroTech\r
- Designation: I280F\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-KBA_I301.eng\r
- Manufacturer: Kosdon by AeroTech\r
- Designation: I301W\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Mark Koelsch\r
-\r
-KBA_I310.eng\r
- Manufacturer: Kosdon by AeroTech\r
- Designation: I310S\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-KBA_I370.eng\r
- Manufacturer: Kosdon by AeroTech\r
- Designation: I370F\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-KBA_I450.eng\r
- Manufacturer: Kosdon by AeroTech\r
- Designation: I450F\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-KBA_I550.eng\r
- Manufacturer: Kosdon by AeroTech\r
- Designation: I550R\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Mark Koelsch\r
-\r
-KBA_J405.eng\r
- Manufacturer: Kosdon by AeroTech\r
- Designation: J405S\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-KBA_J605.eng\r
- Manufacturer: Kosdon by AeroTech\r
- Designation: J605F\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-KBA_K1750.eng\r
- Manufacturer: Kosdon by AeroTech\r
- Designation: K1750R\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Mark Koelsch\r
-\r
-KBA_K400.eng\r
- Manufacturer: Kosdon by AeroTech\r
- Designation: K400S\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-KBA_K600.eng\r
- Manufacturer: Kosdon by AeroTech\r
- Designation: K600F\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-KBA_K750.eng\r
- Manufacturer: Kosdon by AeroTech\r
- Designation: K750W\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Mark Koelsch\r
-\r
-KBA_L1000.eng\r
- Manufacturer: Kosdon by AeroTech\r
- Designation: L1000S\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-KBA_L1400.eng\r
- Manufacturer: Kosdon by AeroTech\r
- Designation: L1400F\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-KBA_M1450.eng\r
- Manufacturer: Kosdon by AeroTech\r
- Designation: M1450W\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Mark Koelsch\r
-\r
-Loki_H144.eng\r
- Manufacturer: Loki Research\r
- Designation: H144-LW\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: William Carney\r
-\r
-Loki_H500.eng\r
- Manufacturer: Loki Research\r
- Designation: H500\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Loki_I405.eng\r
- Manufacturer: Loki Research\r
- Designation: I405LW\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: William Carney\r
-\r
-Loki_J525.eng\r
- Manufacturer: Loki Research\r
- Designation: J525LW\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: William Carney\r
-\r
-Loki_J528.eng\r
- Manufacturer: Loki Research\r
- Designation: J528LW\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: William Carney\r
-\r
-Loki_K250.eng\r
- Manufacturer: Loki Research\r
- Designation: K250LWM\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: William Carney\r
-\r
-Loki_K350.eng\r
- Manufacturer: Loki Research\r
- Designation: K350LWM\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: William Carney\r
-\r
-Loki_K960.eng\r
- Manufacturer: Loki Research\r
- Designation: K960LWB\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: William Carney\r
-\r
-Loki_L1400.eng\r
- Manufacturer: Loki Research\r
- Designation: L1400LW\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: William Carney\r
-\r
-Loki_L930.eng\r
- Manufacturer: Loki Research\r
- Designation: L930LWB\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: William Carney\r
-\r
-Loki_M1882.eng\r
- Manufacturer: Loki Research\r
- Designation: M1882LW\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: William Carney\r
-\r
-PML_F50.eng\r
- Manufacturer: Public Missiles, Ltd.\r
- Designation: F50T\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Mark Koelsch\r
-\r
-PML_G40.eng\r
- Manufacturer: Public Missiles, Ltd.\r
- Designation: G40W\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Mark Koelsch\r
-\r
-PML_G80.eng\r
- Manufacturer: Public Missiles, Ltd.\r
- Designation: G80T\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Mark Koelsch\r
-\r
-PP_H70.eng\r
- Manufacturer: Propulsion Polymers\r
- Designation: 240NS-H70\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-PP_I160.eng\r
- Manufacturer: Propulsion Polymers\r
- Designation: 484NS-I160\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-PP_I80.eng\r
- Manufacturer: Propulsion Polymers\r
- Designation: 460NS-I80\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-PP_J140.eng\r
- Manufacturer: Propulsion Polymers\r
- Designation: 664NS-J140\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Quest_A6.eng\r
- Manufacturer: Quest Aerospace\r
- Designation: A6\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Quest_B6.eng\r
- Manufacturer: Quest Aerospace\r
- Designation: B6\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-Quest_C6.eng\r
- Manufacturer: Quest Aerospace\r
- Designation: C6\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Mark Koelsch\r
-\r
-Quest_D5.eng\r
- Manufacturer: Quest Aerospace\r
- Designation: D5-P\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Mark Koelsch\r
-\r
-RATT_H70.eng\r
- Manufacturer: R.A.T.T. Works Precision Rocket Motors\r
- Designation: H70\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-RATT_I80.eng\r
- Manufacturer: R.A.T.T. Works Precision Rocket Motors\r
- Designation: I80\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-RATT_I90.eng\r
- Manufacturer: R.A.T.T. Works Precision Rocket Motors\r
- Designation: I90L\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-RATT_J160.eng\r
- Manufacturer: R.A.T.T. Works Precision Rocket Motors\r
- Designation: J160\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-RATT_K240.eng\r
- Manufacturer: R.A.T.T. Works Precision Rocket Motors\r
- Designation: K240H\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: John Coker\r
-\r
-RATT_L600.eng\r
- Manufacturer: R.A.T.T. Works Precision Rocket Motors\r
- Designation: L600\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-RATT_M900.eng\r
- Manufacturer: R.A.T.T. Works Precision Rocket Motors\r
- Designation: M900\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-RV_F32.eng\r
- Manufacturer: Rocketvision Flight-Star\r
- Designation: F32\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-RV_F72.eng\r
- Manufacturer: Rocketvision Flight-Star\r
- Designation: F72\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Mark Koelsch\r
-\r
-RV_G55.eng\r
- Manufacturer: Rocketvision Flight-Star\r
- Designation: G55\r
- Data Format: RASP\r
- Data Source: cert\r
- Contributor: Mark Koelsch\r
-\r
-Roadrunner_E25.eng\r
- Manufacturer: Roadrunner Rocketry\r
- Designation: E25\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Roadrunner Rocketry\r
-\r
-Roadrunner_F35.eng\r
- Manufacturer: Roadrunner Rocketry\r
- Designation: F35\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Roadrunner Rocketry\r
-\r
-Roadrunner_F45.eng\r
- Manufacturer: Roadrunner Rocketry\r
- Designation: F45\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Roadrunner Rocketry\r
-\r
-Roadrunner_F60.eng\r
- Manufacturer: Roadrunner Rocketry\r
- Designation: F60\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Roadrunner Rocketry\r
-\r
-Roadrunner_G80.eng\r
- Manufacturer: Roadrunner Rocketry\r
- Designation: G80\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Roadrunner Rocketry\r
-\r
-SkyR_G125.eng\r
- Manufacturer: Sky Ripper Systems\r
- Designation: G125\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-SkyR_G63.eng\r
- Manufacturer: Sky Ripper Systems\r
- Designation: G63\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-SkyR_G69.eng\r
- Manufacturer: Sky Ripper Systems\r
- Designation: G69\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-SkyR_H124.eng\r
- Manufacturer: Sky Ripper Systems\r
- Designation: H124\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Andrew MacMillen\r
-\r
-SkyR_H155.eng\r
- Manufacturer: Sky Ripper Systems\r
- Designation: H155\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Andrew MacMillen\r
-\r
-SkyR_H78.eng\r
- Manufacturer: Sky Ripper Systems\r
- Designation: H78\r
- Data Format: RASP\r
- Data Source: user\r
- Contributor: John Coker\r
-\r
-SkyR_I117.eng\r
- Manufacturer: Sky Ripper Systems\r
- Designation: I117\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Andrew MacMillen\r
-\r
-SkyR_I119.eng\r
- Manufacturer: Sky Ripper Systems\r
- Designation: I119\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Andrew MacMillen\r
-\r
-SkyR_I147.eng\r
- Manufacturer: Sky Ripper Systems\r
- Designation: I147\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Andrew MacMillen\r
-\r
-SkyR_J144.eng\r
- Manufacturer: Sky Ripper Systems\r
- Designation: J144\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Andrew MacMillen\r
-\r
-SkyR_J261.eng\r
- Manufacturer: Sky Ripper Systems\r
- Designation: J261G\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: John Coker\r
-\r
-SkyR_J263.eng\r
- Manufacturer: Sky Ripper Systems\r
- Designation: J263G\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: John Coker\r
-\r
-SkyR_J337.eng\r
- Manufacturer: Sky Ripper Systems\r
- Designation: J337B\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: John Coker\r
-\r
-SkyR_J348.eng\r
- Manufacturer: Sky Ripper Systems\r
- Designation: J348B\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: John Coker\r
-\r
-SkyR_K257.eng\r
- Manufacturer: Sky Ripper Systems\r
- Designation: K257G\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: John Coker\r
-\r
-SkyR_K347.eng\r
- Manufacturer: Sky Ripper Systems\r
- Designation: K347B\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: John Coker\r
-\r
-WCH_I110.eng\r
- Manufacturer: West Coast Hybrids\r
- Designation: 499 I110-P\r
- Data Format: RASP\r
- Data Source: mfr\r
- Contributor: Andrew MacMillen\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Animal Motor Works" code="I195WW" Type="reloadable" dia="38." len="249."\r
+initWt="495." propWt="193." delays="18" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="185.064" peakThrust="231.607" throatDia="0." exitDia="0."\r
+Itot="349.772" burn-time="1.89" massFrac="38.99" Isp="184.8" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Animal Motor Works 38-390</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="193." cg="124.5"/>\r
+ <eng-data t="0.002" f="10.548" m="192.994" cg="124.5"/>\r
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+ <eng-data t="1.89" f="0." m="0." cg="124.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;Animal Motor Works 38-390\r
-I220SK 38 249 20 0.202 0.495 AMW\r
- 0.0050 12.747\r
- 0.019 45.25\r
- 0.036 79.666\r
- 0.052 125.554\r
- 0.069 162.519\r
- 0.076 169.53\r
- 0.095 174.629\r
- 0.167 176.541\r
- 0.229 191.199\r
- 0.447 235.175\r
- 0.602 260.668\r
- 0.733 288.073\r
- 0.85 302.095\r
- 0.974 301.457\r
- 1.094 289.985\r
- 1.184 268.954\r
- 1.268 240.273\r
- 1.302 219.879\r
- 1.388 177.178\r
- 1.418 147.224\r
- 1.435 127.467\r
- 1.473 91.139\r
- 1.504 65.645\r
- 1.543 40.789\r
- 1.593 19.12\r
- 1.622 10.197\r
- 1.65 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Animal Motor Works" code="I220SK" Type="reloadable" dia="38." len="249."\r
+initWt="495." propWt="202." delays="20" auto-calc-mass="1" auto-calc-cg="1"\r
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+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Animal Motor Works 38-390</comments>\r
+ <data>\r
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+ <eng-data t="1.65" f="0." m="0." cg="124.5"/>\r
+ </data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; AMW 38-390\r
-I271BB 38 258 0 0.189 0.493 AMW\r
-0.011 119.530\r
-0.035 213.907\r
-0.050 245.903\r
-0.074 262.705\r
-0.115 269.446\r
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-0.346 282.929\r
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-0.916 318.245\r
-1.054 324.986\r
-1.162 331.400\r
-1.201 326.696\r
-1.225 313.214\r
-1.242 286.249\r
-1.268 240.990\r
-1.294 188.888\r
-1.323 136.833\r
-1.346 87.565\r
-1.368 45.467\r
-1.392 18.523\r
-1.430 0.000\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Animal Motor Works" code="I271BB" Type="reloadable" dia="38." len="258."\r
+initWt="493." propWt="189." delays="20" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="272.271" peakThrust="331.4" throatDia="0." exitDia="0." Itot="389.348"\r
+burn-time="1.43" massFrac="38.34" Isp="210.07" tDiv="10" tStep="-1." tFix="1"\r
+FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+<comments>AMW 38-390</comments>\r
+<data>\r
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+ <eng-data t="1.43" f="0." m="0." cg="129."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; AMW 38-390\r
-I285GG 38 258 0 0.206 0.515 AMW\r
-0.013 61.575\r
-0.032 119.327\r
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-0.076 191.004\r
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-0.456 267.686\r
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-0.716 289.358\r
-0.841 291.200\r
-0.936 290.310\r
-1.051 285.204\r
-1.139 277.696\r
-1.204 280.199\r
-1.243 278.998\r
-1.265 268.887\r
-1.286 242.559\r
-1.319 187.200\r
-1.359 134.443\r
-1.387 86.702\r
-1.407 52.776\r
-1.428 31.413\r
-1.448 16.337\r
-1.465 5.026\r
-1.480 0.000\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Animal Motor Works" code="I285GG" Type="reloadable" dia="38." len="258."\r
+initWt="515." propWt="206." delays="20" auto-calc-mass="1" auto-calc-cg="1"\r
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+FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+<comments>AMW 38-390</comments>\r
+<data>\r
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+<eng-data t="1.48" f="0." m="0." cg="129."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; This file my be used or given away. All I ask is that this header \r
-; is maintained to give credit to NAR S&T. Thank you, Jack Kane\r
-; The total impulse, peak thrust, average thrust and burn time are\r
-; the same as the averaged static test data on the NAR web site in\r
-; the certification file. The curve drawn with these data points is as\r
-; close to the certification curve as can be with such a limited \r
-; number of points (32) allowed with wRASP up to v1.6.\r
-;Animal Motor Works 38-640 \r
-I315SK 38 369 20 0.3829 0.7166 AMW\r
-0.011 314.573\r
-0.030 312.796\r
-0.066 300.786\r
-0.084 300.502\r
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-0.447 347.855\r
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-0.901 384.836\r
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-1.082 378.323\r
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-1.536 202.733\r
-1.627 90.867\r
-1.718 35.427\r
-1.808 8.192\r
-1.815 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="148.78" Itot="558.679" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="308.662" burn-time="1.81" cgDiv="10" cgFix="1" cgStep="-1." code="I315SK" delays="20" dia="38." exitDia="0." initWt="716.6" len="369." mDiv="10" mFix="1" mStep="-1." massFrac="53.43" mfg="Animal Motor Works" peakThrust="385.59" propWt="382.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="184.5" f="0." m="382.9" t="0."/>\r
+<eng-data cg="184.5" f="314.57" m="381.822" t="0.01"/>\r
+<eng-data cg="184.5" f="312.8" m="377.522" t="0.03"/>\r
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+<eng-data cg="184.5" f="347.12" m="51.5062" t="1.36"/>\r
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+<eng-data cg="184.5" f="202.73" m="14.2957" t="1.54"/>\r
+<eng-data cg="184.5" f="90.87" m="5.24059" t="1.63"/>\r
+<eng-data cg="184.5" f="35.43" m="1.34531" t="1.72"/>\r
+<eng-data cg="184.5" f="8.19" m="0." t="1.81"/>\r
+<eng-data cg="184.5" f="0." m="0." t="1.81"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Animal Motor Works" code="I325WW" Type="reloadable" dia="38." len="370."\r
+initWt="712." propWt="317." delays="18" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="306.99" peakThrust="388.611" throatDia="0." exitDia="0."\r
+Itot="583.589" burn-time="1.9" massFrac="44.52" Isp="187.73" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Animal Motor Works 38-640</comments>\r
+<data>\r
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+<eng-data t="0.014" f="68.71" m="316.739" cg="185."/>\r
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+<eng-data t="0.252" f="373.836" m="272.069" cg="185."/>\r
+<eng-data t="0.35" f="381.224" m="251.972" cg="185."/>\r
+<eng-data t="0.47" f="382.701" m="227.075" cg="185."/>\r
+<eng-data t="0.622" f="388.611" m="195.233" cg="185."/>\r
+<eng-data t="1.102" f="384.179" m="94.4879" cg="185."/>\r
+<eng-data t="1.366" f="364.971" m="40.773" cg="185."/>\r
+<eng-data t="1.379" f="360.537" m="38.2114" cg="185."/>\r
+<eng-data t="1.415" f="331.724" m="31.4429" cg="185."/>\r
+<eng-data t="1.49" f="223.119" m="20.1409" cg="185."/>\r
+<eng-data t="1.505" f="211.298" m="18.3711" cg="185."/>\r
+<eng-data t="1.551" f="187.657" m="13.3868" cg="185."/>\r
+<eng-data t="1.592" f="162.538" m="9.48725" cg="185."/>\r
+<eng-data t="1.688" f="80.529" m="3.14973" cg="185."/>\r
+<eng-data t="1.726" f="50.978" m="1.79249" cg="185."/>\r
+<eng-data t="1.775" f="27.336" m="0.750276" cg="185."/>\r
+<eng-data t="1.806" f="16.993" m="0.37705" cg="185."/>\r
+<eng-data t="1.834" f="9.605" m="0.174781" cg="185."/>\r
+<eng-data t="1.901" f="0." m="0." cg="185."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works 38-640 \r
-I375GG 38 369 20 0.3936 0.7338 AMW\r
-0.013 223.878\r
-0.045 273.929\r
-0.092 312.421\r
-0.140 334.383\r
-0.219 357.983\r
-0.298 381.992\r
-0.377 410.267\r
-0.457 431.141\r
-0.536 454.458\r
-0.615 476.825\r
-0.694 495.473\r
-0.773 504.665\r
-0.852 510.942\r
-0.931 511.972\r
-1.011 489.639\r
-1.090 441.350\r
-1.169 392.762\r
-1.248 354.753\r
-1.327 292.385\r
-1.406 177.309\r
-1.486 63.879\r
-1.565 14.901\r
-1.583 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="152.41" Itot="588.308" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="372.347" burn-time="1.58" cgDiv="10" cgFix="1" cgStep="-1." code="I375GG" delays="20" dia="38." exitDia="0." initWt="733.8" len="369." mDiv="10" mFix="1" mStep="-1." massFrac="53.64" mfg="Animal Motor Works" peakThrust="511.97" propWt="393.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="184.5" f="0." m="393.6" t="0."/>\r
+<eng-data cg="184.5" f="223.88" m="392.851" t="0.01"/>\r
+<eng-data cg="184.5" f="273.93" m="387.855" t="0.04"/>\r
+<eng-data cg="184.5" f="312.42" m="378.048" t="0.09"/>\r
+<eng-data cg="184.5" f="334.38" m="367.23" t="0.14"/>\r
+<eng-data cg="184.5" f="357.98" m="348.701" t="0.22"/>\r
+<eng-data cg="184.5" f="381.99" m="328.898" t="0.3"/>\r
+<eng-data cg="184.5" f="410.27" m="307.696" t="0.38"/>\r
+<eng-data cg="184.5" f="431.14" m="285.179" t="0.46"/>\r
+<eng-data cg="184.5" f="454.46" m="261.479" t="0.54"/>\r
+<eng-data cg="184.5" f="476.82" m="239.672" t="0.61"/>\r
+<eng-data cg="184.5" f="495.47" m="213.652" t="0.69"/>\r
+<eng-data cg="184.5" f="504.67" m="186.887" t="0.77"/>\r
+<eng-data cg="184.5" f="510.94" m="159.707" t="0.85"/>\r
+<eng-data cg="184.5" f="511.97" m="132.333" t="0.93"/>\r
+<eng-data cg="184.5" f="489.64" m="105.528" t="1.01"/>\r
+<eng-data cg="184.5" f="441.35" m="80.6134" t="1.09"/>\r
+<eng-data cg="184.5" f="392.76" m="58.2913" t="1.17"/>\r
+<eng-data cg="184.5" f="354.75" m="38.2868" t="1.25"/>\r
+<eng-data cg="184.5" f="292.38" m="20.9686" t="1.33"/>\r
+<eng-data cg="184.5" f="177.31" m="8.39903" t="1.41"/>\r
+<eng-data cg="184.5" f="63.88" m="1.94442" t="1.49"/>\r
+<eng-data cg="184.5" f="14.9" m="0.0996866" t="1.56"/>\r
+<eng-data cg="184.5" f="0." m="0." t="1.58"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+; Kosdon J230 RASP.ENG file made from NAR published data\r
+; File produced November 1, 2000\r
+; The total impulse, peak thrust, average thrust and burn time are\r
+; the same as the averaged static test data on the NAR web site in\r
+; the certification file. The curve drawn with these data points is as\r
+; close to the certification curve as can be with such a limited\r
+; number of points (32) allowed with wRASP up to v1.6.\r
+J230 54 326 8 .5008 1.1690 K\r
+0.026 146.964\r
+0.039 214.239\r
+0.076 239.367\r
+0.161 247.777\r
+0.306 247.677\r
+0.488 249.679\r
+0.754 260.090\r
+0.948 268.400\r
+1.227 274.607\r
+1.590 276.720\r
+1.905 270.102\r
+2.195 267.899\r
+2.498 259.390\r
+2.643 252.982\r
+2.824 248.778\r
+3.115 242.270\r
+3.369 229.656\r
+3.478 221.147\r
+3.550 204.328\r
+3.610 170.690\r
+3.658 126.541\r
+3.718 82.442\r
+3.790 61.418\r
+3.899 40.365\r
+3.983 17.229\r
+4.080 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Animal Motor Works" code="J230SK" Type="reloadable" dia="54." len="326."\r
+initWt="1183.53" propWt="525." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="227.973" peakThrust="277.759" throatDia="0." exitDia="0."\r
+Itot="768.724" burn-time="3.37" massFrac="44.36" Isp="149.31" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve from the AMW motor assembly instructions and\r
+CAR/NAR/TRA certified rocket motor list dated 9/28/08. The total weight was\r
+provided by Paul Robinson of AMW.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="525." cg="163."/>\r
+<eng-data t="0.033" f="219.31" m="522.529" cg="163."/>\r
+<eng-data t="0.048" f="257.069" m="520.089" cg="163."/>\r
+<eng-data t="0.059" f="271.034" m="518.105" cg="163."/>\r
+<eng-data t="0.084" f="271.034" m="513.477" cg="163."/>\r
+<eng-data t="0.132" f="263.276" m="504.72" cg="163."/>\r
+<eng-data t="0.176" f="253.966" m="496.948" cg="163."/>\r
+<eng-data t="0.216" f="237.414" m="490.236" cg="163."/>\r
+<eng-data t="0.246" f="228.621" m="485.462" cg="163."/>\r
+<eng-data t="0.29" f="225." m="478.647" cg="163."/>\r
+<eng-data t="0.337" f="225." m="471.424" cg="163."/>\r
+<eng-data t="0.421" f="229.138" m="458.398" cg="163."/>\r
+<eng-data t="0.59" f="234.828" m="431.623" cg="163."/>\r
+<eng-data t="0.788" f="243.621" m="399.274" cg="163."/>\r
+<eng-data t="0.96" f="248.276" m="370.383" cg="163."/>\r
+<eng-data t="1.096" f="256.552" m="346.938" cg="163."/>\r
+<eng-data t="1.231" f="255.517" m="323.333" cg="163."/>\r
+<eng-data t="1.374" f="261.724" m="298.075" cg="163."/>\r
+<eng-data t="1.646" f="270." m="248.688" cg="163."/>\r
+<eng-data t="1.799" f="275.172" m="220.205" cg="163."/>\r
+<eng-data t="1.851" f="277.759" m="210.387" cg="163."/>\r
+<eng-data t="1.906" f="273.621" m="200.031" cg="163."/>\r
+<eng-data t="1.957" f="270.517" m="190.555" cg="163."/>\r
+<eng-data t="2.027" f="273.103" m="177.561" cg="163."/>\r
+<eng-data t="2.078" f="272.069" m="168.067" cg="163."/>\r
+<eng-data t="2.144" f="272.069" m="155.803" cg="163."/>\r
+<eng-data t="2.228" f="271.552" m="140.21" cg="163."/>\r
+<eng-data t="2.28" f="271.552" m="130.566" cg="163."/>\r
+<eng-data t="2.316" f="267.414" m="123.941" cg="163."/>\r
+<eng-data t="2.379" f="263.793" m="112.513" cg="163."/>\r
+<eng-data t="2.43" f="259.655" m="103.397" cg="163."/>\r
+<eng-data t="2.551" f="240.517" m="82.7305" cg="163."/>\r
+<eng-data t="2.752" f="211.034" m="51.7377" cg="163."/>\r
+<eng-data t="2.837" f="200.69" m="39.7872" cg="163."/>\r
+<eng-data t="2.888" f="196.034" m="32.8782" cg="163."/>\r
+<eng-data t="2.914" f="199.138" m="29.3697" cg="163."/>\r
+<eng-data t="2.939" f="206.379" m="25.9079" cg="163."/>\r
+<eng-data t="2.961" f="215.172" m="22.741" cg="163."/>\r
+<eng-data t="2.983" f="219.828" m="19.4731" cg="163."/>\r
+<eng-data t="3.016" f="206.379" m="14.6703" cg="163."/>\r
+<eng-data t="3.057" f="158.276" m="9.56496" cg="163."/>\r
+<eng-data t="3.093" f="113.793" m="6.22039" cg="163."/>\r
+<eng-data t="3.145" f="69.31" m="2.96909" cg="163."/>\r
+<eng-data t="3.185" f="40.345" m="1.47131" cg="163."/>\r
+<eng-data t="3.236" f="14.483" m="0.516472" cg="163."/>\r
+<eng-data t="3.287" f="5.69" m="0.165154" cg="163."/>\r
+<eng-data t="3.372" f="0." m="0." cg="163."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AMW Animal Motor Works fixed by dberez 12/08/03\r
-;\r
-;Animal Motor Works J357 White Wolf\r
-J357WW 54 326 0 0.5481 1.2101 AMW\r
-0.02 129.64\r
-0.03 205.95\r
-0.05 265.00\r
-0.06 316.51\r
-0.09 326.05\r
-0.13 314.60\r
-0.18 301.25\r
-0.24 299.34\r
-0.35 312.69\r
-0.50 326.05\r
-0.66 333.68\r
-0.87 345.13\r
-1.07 358.48\r
-1.46 383.18\r
-1.77 398.45\r
-1.86 400.36\r
-1.98 402.35\r
-2.18 398.45\r
-2.29 390.82\r
-2.41 369.93\r
-2.51 354.67\r
-2.55 352.76\r
-2.60 347.03\r
-2.65 335.59\r
-2.69 310.79\r
-2.75 249.73\r
-2.81 175.43\r
-2.84 108.65\r
-2.90 53.38\r
-2.92 20.98\r
-2.95 0.00\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="185.87" Itot="999.076" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="338.67" burn-time="2.95" cgDiv="10" cgFix="1" cgStep="-1." code="J357WW" delays="1000" dia="54." exitDia="0." initWt="1210.1" len="326." mDiv="10" mFix="1" mStep="-1." massFrac="45.29" mfg="Animal Motor Works" peakThrust="402.35" propWt="548.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <data>\r
+ <eng-data cg="163." f="0." m="548.1" t="0."/>\r
+ <eng-data cg="163." f="129.64" m="547.389" t="0.02"/>\r
+ <eng-data cg="163." f="205.95" m="546.468" t="0.03"/>\r
+ <eng-data cg="163." f="265." m="543.885" t="0.05"/>\r
+ <eng-data cg="163." f="316.51" m="542.289" t="0.06"/>\r
+ <eng-data cg="163." f="326.05" m="537.002" t="0.09"/>\r
+ <eng-data cg="163." f="314.6" m="529.972" t="0.13"/>\r
+ <eng-data cg="163." f="301.25" m="521.526" t="0.18"/>\r
+ <eng-data cg="163." f="299.34" m="511.641" t="0.24"/>\r
+ <eng-data cg="163." f="312.69" m="493.174" t="0.35"/>\r
+ <eng-data cg="163." f="326.05" m="466.893" t="0.5"/>\r
+ <eng-data cg="163." f="333.68" m="437.938" t="0.66"/>\r
+ <eng-data cg="163." f="345.13" m="398.836" t="0.87"/>\r
+ <eng-data cg="163." f="358.48" m="360.236" t="1.07"/>\r
+ <eng-data cg="163." f="383.18" m="280.894" t="1.46"/>\r
+ <eng-data cg="163." f="398.45" m="214.429" t="1.77"/>\r
+ <eng-data cg="163." f="400.36" m="194.709" t="1.86"/>\r
+ <eng-data cg="163." f="402.35" m="168.286" t="1.98"/>\r
+ <eng-data cg="163." f="398.45" m="124.354" t="2.18"/>\r
+ <eng-data cg="163." f="390.82" m="100.539" t="2.29"/>\r
+ <eng-data cg="163." f="369.93" m="75.4978" t="2.41"/>\r
+ <eng-data cg="163." f="354.67" m="55.6218" t="2.51"/>\r
+ <eng-data cg="163." f="352.76" m="47.8597" t="2.55"/>\r
+ <eng-data cg="163." f="347.03" m="38.262" t="2.6"/>\r
+ <eng-data cg="163." f="335.59" m="28.8997" t="2.65"/>\r
+ <eng-data cg="163." f="310.79" m="21.8076" t="2.69"/>\r
+ <eng-data cg="163." f="249.73" m="12.5824" t="2.75"/>\r
+ <eng-data cg="163." f="175.43" m="5.58504" t="2.81"/>\r
+ <eng-data cg="163." f="108.65" m="3.24731" t="2.84"/>\r
+ <eng-data cg="163." f="53.38" m="0.580591" t="2.9"/>\r
+ <eng-data cg="163." f="20.98" m="0.172647" t="2.92"/>\r
+ <eng-data cg="163." f="0." m="0." t="2.95"/>\r
+ </data>\r
+ </engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works 54-1400 \r
-J365SK 54 403 0 0.7571 1.4593 AMW\r
-0.029 389.731\r
-0.123 360.219\r
-0.218 334.200\r
-0.376 326.150\r
-0.534 334.217\r
-0.692 341.669\r
-0.850 347.676\r
-1.007 359.408\r
-1.165 370.043\r
-1.323 383.343\r
-1.481 399.248\r
-1.639 417.477\r
-1.797 443.735\r
-1.955 472.683\r
-2.112 501.668\r
-2.270 497.077\r
-2.428 425.371\r
-2.586 349.017\r
-2.744 262.068\r
-2.902 107.073\r
-3.060 41.821\r
-3.157 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="148.91" Itot="1105.56" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="349.861" burn-time="3.16" cgDiv="10" cgFix="1" cgStep="-1." code="J365SK" delays="1000" dia="54." exitDia="0." initWt="1459.3" len="403." mDiv="10" mFix="1" mStep="-1." massFrac="51.88" mfg="Animal Motor Works" peakThrust="501.67" propWt="757.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="201.5" f="0." m="757.1" t="0."/>\r
+<eng-data cg="201.5" f="389.73" m="753.097" t="0.03"/>\r
+<eng-data cg="201.5" f="360.22" m="729.986" t="0.12"/>\r
+<eng-data cg="201.5" f="334.2" m="706.209" t="0.22"/>\r
+<eng-data cg="201.5" f="326.15" m="670.031" t="0.38"/>\r
+<eng-data cg="201.5" f="334.22" m="636.114" t="0.53"/>\r
+<eng-data cg="201.5" f="341.67" m="599.086" t="0.69"/>\r
+<eng-data cg="201.5" f="347.68" m="561.32" t="0.85"/>\r
+<eng-data cg="201.5" f="359.41" m="522.582" t="1.01"/>\r
+<eng-data cg="201.5" f="370.04" m="482.619" t="1.17"/>\r
+<eng-data cg="201.5" f="383.34" m="443.925" t="1.32"/>\r
+<eng-data cg="201.5" f="399.25" m="401.051" t="1.48"/>\r
+<eng-data cg="201.5" f="417.48" m="356.307" t="1.64"/>\r
+<eng-data cg="201.5" f="443.74" m="309.125" t="1.8"/>\r
+<eng-data cg="201.5" f="472.68" m="258.919" t="1.96"/>\r
+<eng-data cg="201.5" f="501.67" m="208.876" t="2.11"/>\r
+<eng-data cg="201.5" f="497.08" m="154.159" t="2.27"/>\r
+<eng-data cg="201.5" f="425.37" m="103.623" t="2.43"/>\r
+<eng-data cg="201.5" f="349.02" m="61.1982" t="2.59"/>\r
+<eng-data cg="201.5" f="262.07" m="29.8121" t="2.74"/>\r
+<eng-data cg="201.5" f="107.07" m="9.58885" t="2.9"/>\r
+<eng-data cg="201.5" f="41.82" m="1.43194" t="3.06"/>\r
+<eng-data cg="201.5" f="0." m="0." t="3.16"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works 54-1050\r
-;AMW J370GG RASP.ENG file made from NAR data\r
-;File produced FEB 20, 2003\r
-;This file my be used or given away. All I ask is that this header\r
-;is maintained to give credit to NAR S&T. Thank you, Jack Kane\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-J370GG 54 326 100 0.5983 1.2491 Animal_Motor_Works \r
-0.008 185.496\r
-0.024 149.516\r
-0.063 225.273\r
-0.087 272.647\r
-0.122 304.829\r
-0.158 304.829\r
-0.273 335.212\r
-0.431 363.796\r
-0.573 390.381\r
-0.707 413.168\r
-0.877 428.459\r
-1.019 441.852\r
-1.126 441.852\r
-1.224 458.46\r
-1.284 443.951\r
-1.386 440.153\r
-1.572 438.454\r
-1.651 438.554\r
-1.813 417.765\r
-2.022 404.673\r
-2.141 385.883\r
-2.212 385.883\r
-2.255 374.59\r
-2.299 387.882\r
-2.362 357.599\r
-2.401 384.184\r
-2.421 348.204\r
-2.457 316.122\r
-2.559 251.758\r
-2.697 115.635\r
-2.753 45.624\r
-2.82 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="175.7" Itot="1030.88" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="365.561" burn-time="2.82" cgDiv="10" cgFix="1" cgStep="-1." code="J370GG" delays="1000" dia="54." exitDia="0." initWt="1249.1" len="326." mDiv="10" mFix="1" mStep="-1." massFrac="47.9" mfg="Animal Motor Works" peakThrust="458.46" propWt="598.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <comments><![CDATA[Animal Motor Works 54-1050\r
+AMW J370GG RASP.ENG file made from NAR data\r
+File produced FEB 20, 2003\r
+This file my be used or given away. All I ask is that this header\r
+is maintained to give credit to NAR S&T. Thank you, Jack Kane\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+]]></comments>\r
+ <data>\r
+ <eng-data cg="163." f="0." m="598.3" t="0."/>\r
+ <eng-data cg="163." f="185.496" m="597.869" t="0.008"/>\r
+ <eng-data cg="163." f="149.516" m="596.314" t="0.024"/>\r
+ <eng-data cg="163." f="225.273" m="592.072" t="0.063"/>\r
+ <eng-data cg="163." f="272.647" m="588.605" t="0.087"/>\r
+ <eng-data cg="163." f="304.829" m="582.739" t="0.122"/>\r
+ <eng-data cg="163." f="304.829" m="576.37" t="0.158"/>\r
+ <eng-data cg="163." f="335.212" m="555.011" t="0.273"/>\r
+ <eng-data cg="163." f="363.796" m="522.962" t="0.431"/>\r
+ <eng-data cg="163." f="390.381" m="491.885" t="0.573"/>\r
+ <eng-data cg="163." f="413.168" m="460.639" t="0.707"/>\r
+ <eng-data cg="163." f="428.459" m="419.119" t="0.877"/>\r
+ <eng-data cg="163." f="441.852" m="383.257" t="1.019"/>\r
+ <eng-data cg="163." f="441.852" m="355.818" t="1.126"/>\r
+ <eng-data cg="163." f="458.46" m="330.214" t="1.224"/>\r
+ <eng-data cg="163." f="443.951" m="314.502" t="1.284"/>\r
+ <eng-data cg="163." f="440.153" m="288.333" t="1.386"/>\r
+ <eng-data cg="163." f="438.454" m="240.91" t="1.572"/>\r
+ <eng-data cg="163." f="438.554" m="220.805" t="1.651"/>\r
+ <eng-data cg="163." f="417.765" m="180.549" t="1.813"/>\r
+ <eng-data cg="163." f="404.673" m="130.669" t="2.022"/>\r
+ <eng-data cg="163." f="385.883" m="103.369" t="2.141"/>\r
+ <eng-data cg="163." f="385.883" m="87.4681" t="2.212"/>\r
+ <eng-data cg="163." f="374.59" m="77.9789" t="2.255"/>\r
+ <eng-data cg="163." f="387.882" m="68.2434" t="2.299"/>\r
+ <eng-data cg="163." f="357.599" m="54.6147" t="2.362"/>\r
+ <eng-data cg="163." f="384.184" m="46.2197" t="2.401"/>\r
+ <eng-data cg="163." f="348.204" m="41.969" t="2.421"/>\r
+ <eng-data cg="163." f="316.122" m="35.029" t="2.457"/>\r
+ <eng-data cg="163." f="251.758" m="18.2202" t="2.559"/>\r
+ <eng-data cg="163." f="115.635" m="3.50759" t="2.697"/>\r
+ <eng-data cg="163." f="45.624" m="0.887049" t="2.753"/>\r
+ <eng-data cg="163." f="0." m="0." t="2.82"/>\r
+ </data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;AMW J400 RASP.ENG file made from NAR published data\r
-;File produced April 19, 2004\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-J400RR 54 326 100 0.558 1.2314 Animal_Motor_Works \r
-0.043 246.55\r
-0.06 317.381\r
-0.081 344.709\r
-0.107 358.372\r
-0.15 356.06\r
-0.201 365.204\r
-0.308 392.532\r
-0.568 435.734\r
-0.863 458.339\r
-1.094 469.24\r
-1.209 467.18\r
-1.466 460.148\r
-1.705 443.972\r
-1.923 423.275\r
-2.132 409.411\r
-2.303 413.831\r
-2.402 420.563\r
-2.47 413.831\r
-2.517 395.445\r
-2.543 347.421\r
-2.568 265.238\r
-2.598 128.198\r
-2.615 68.801\r
-2.632 25.398\r
-2.66 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="200.08" Itot="1094.88" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="411.61" burn-time="2.66" cgDiv="10" cgFix="1" cgStep="-1." code="J400RR" delays="1000" dia="54." exitDia="0." initWt="1231.4" len="326." mDiv="10" mFix="1" mStep="-1." massFrac="45.31" mfg="Animal Motor Works" peakThrust="469.24" propWt="558." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW J400 RASP.ENG file made from NAR published data\r
+File produced April 19, 2004\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+ <eng-data cg="163." f="0." m="558." t="0."/>\r
+ <eng-data cg="163." f="246.55" m="555.298" t="0.043"/>\r
+ <eng-data cg="163." f="317.381" m="552.856" t="0.06"/>\r
+ <eng-data cg="163." f="344.709" m="549.313" t="0.081"/>\r
+ <eng-data cg="163." f="358.372" m="544.654" t="0.107"/>\r
+ <eng-data cg="163." f="356.06" m="536.826" t="0.15"/>\r
+ <eng-data cg="163." f="365.204" m="527.453" t="0.201"/>\r
+ <eng-data cg="163." f="392.532" m="506.792" t="0.308"/>\r
+ <eng-data cg="163." f="435.734" m="451.916" t="0.568"/>\r
+ <eng-data cg="163." f="458.339" m="384.707" t="0.863"/>\r
+ <eng-data cg="163." f="469.24" m="330.106" t="1.094"/>\r
+ <eng-data cg="163." f="467.18" m="302.665" t="1.209"/>\r
+ <eng-data cg="163." f="460.148" m="241.935" t="1.466"/>\r
+ <eng-data cg="163." f="443.972" m="186.871" t="1.705"/>\r
+ <eng-data cg="163." f="423.275" m="138.695" t="1.923"/>\r
+ <eng-data cg="163." f="409.411" m="94.3478" t="2.132"/>\r
+ <eng-data cg="163." f="413.831" m="58.4754" t="2.303"/>\r
+ <eng-data cg="163." f="420.563" m="37.4258" t="2.402"/>\r
+ <eng-data cg="163." f="413.831" m="22.9675" t="2.47"/>\r
+ <eng-data cg="163." f="395.445" m="13.2751" t="2.517"/>\r
+ <eng-data cg="163." f="347.421" m="8.35334" t="2.543"/>\r
+ <eng-data cg="163." f="265.238" m="4.45036" t="2.568"/>\r
+ <eng-data cg="163." f="128.198" m="1.44268" t="2.598"/>\r
+ <eng-data cg="163." f="68.801" m="0.589283" t="2.615"/>\r
+ <eng-data cg="163." f="25.398" m="0.181215" t="2.632"/>\r
+ <eng-data cg="163." f="0." m="0." t="2.66"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;Animal Motor Works 38-640 \r
-J440BB 38 369 20 0.3853 0.6985 AMW\r
-0.007 468.505\r
-0.022 509.996\r
-0.037 527.687\r
-0.052 532.792\r
-0.082 530.181\r
-0.127 525.586\r
-0.202 521.566\r
-0.277 519.840\r
-0.352 521.522\r
-0.426 525.414\r
-0.501 531.248\r
-0.576 538.724\r
-0.651 541.761\r
-0.726 538.508\r
-0.801 531.072\r
-0.876 516.175\r
-0.950 494.942\r
-1.025 477.251\r
-1.100 433.297\r
-1.175 313.900\r
-1.250 187.467\r
-1.325 101.546\r
-1.400 45.751\r
-1.474 22.083\r
-1.497 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="167.98" Itot="634.714" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="423.143" burn-time="1.5" cgDiv="10" cgFix="1" cgStep="-1." code="J440BB" delays="20" dia="38." exitDia="0." initWt="698.5" len="369." mDiv="10" mFix="1" mStep="-1." massFrac="55.16" mfg="Animal Motor Works" peakThrust="541.76" propWt="385.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="184.5" f="0." m="385.3" t="0."/>\r
+<eng-data cg="184.5" f="468.51" m="383.878" t="0.01"/>\r
+<eng-data cg="184.5" f="510." m="380.908" t="0.02"/>\r
+<eng-data cg="184.5" f="527.69" m="374.609" t="0.04"/>\r
+<eng-data cg="184.5" f="532.79" m="371.39" t="0.05"/>\r
+<eng-data cg="184.5" f="530.18" m="361.711" t="0.08"/>\r
+<eng-data cg="184.5" f="525.59" m="345.688" t="0.13"/>\r
+<eng-data cg="184.5" f="521.57" m="323.44" t="0.2"/>\r
+<eng-data cg="184.5" f="519.84" m="298.153" t="0.28"/>\r
+<eng-data cg="184.5" f="521.52" m="276.027" t="0.35"/>\r
+<eng-data cg="184.5" f="525.41" m="250.606" t="0.43"/>\r
+<eng-data cg="184.5" f="531.25" m="228.155" t="0.5"/>\r
+<eng-data cg="184.5" f="538.72" m="202.175" t="0.58"/>\r
+<eng-data cg="184.5" f="541.76" m="179.218" t="0.65"/>\r
+<eng-data cg="184.5" f="538.51" m="152.987" t="0.73"/>\r
+<eng-data cg="184.5" f="531.07" m="130.262" t="0.8"/>\r
+<eng-data cg="184.5" f="516.17" m="104.834" t="0.88"/>\r
+<eng-data cg="184.5" f="494.94" m="83.351" t="0.95"/>\r
+<eng-data cg="184.5" f="477.25" m="62.6953" t="1.02"/>\r
+<eng-data cg="184.5" f="433.3" m="40.5855" t="1.1"/>\r
+<eng-data cg="184.5" f="313.9" m="22.4421" t="1.18"/>\r
+<eng-data cg="184.5" f="187.47" m="11.7897" t="1.25"/>\r
+<eng-data cg="184.5" f="101.55" m="4.77183" t="1.33"/>\r
+<eng-data cg="184.5" f="45.75" m="1.64221" t="1.4"/>\r
+<eng-data cg="184.5" f="22.08" m="0.201053" t="1.47"/>\r
+<eng-data cg="184.5" f="0." m="0." t="1.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="204.62" Itot="1069.71" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="459.105" burn-time="2.33" cgDiv="10" cgFix="1" cgStep="-1." code="J450ST" delays="1000" dia="54." exitDia="0." initWt="1196.4" len="326." mDiv="10" mFix="1" mStep="-1." massFrac="44.56" mfg="Animal Motor Works" peakThrust="563.18" propWt="533.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments><![CDATA[Animal Motor Works 54-1050\r
+AMW J450ST RASP.ENG file made from NAR published data\r
+File produced SEPT 4, 2002\r
+This file my be used or given away. All I ask is that this header\r
+is maintained to give credit to NAR S&T. Thank you, Jack Kane\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+]]></comments>\r
+<data>\r
+<eng-data cg="163." f="0." m="533.1" t="0."/>\r
+<eng-data cg="163." f="251.586" m="532.536" t="0.009"/>\r
+<eng-data cg="163." f="376.074" m="531.441" t="0.016"/>\r
+<eng-data cg="163." f="413.45" m="528.687" t="0.03"/>\r
+<eng-data cg="163." f="430.832" m="524.269" t="0.051"/>\r
+<eng-data cg="163." f="423.296" m="515.117" t="0.094"/>\r
+<eng-data cg="163." f="413.149" m="500.944" t="0.162"/>\r
+<eng-data cg="163." f="395.566" m="480.793" t="0.262"/>\r
+<eng-data cg="163." f="420.182" m="452.335" t="0.402"/>\r
+<eng-data cg="163." f="444.898" m="432.288" t="0.495"/>\r
+<eng-data cg="163." f="504.078" m="358.984" t="0.805"/>\r
+<eng-data cg="163." f="536.028" m="296.005" t="1.048"/>\r
+<eng-data cg="163." f="550.597" m="248.622" t="1.223"/>\r
+<eng-data cg="163." f="563.18" m="227.529" t="1.299"/>\r
+<eng-data cg="163." f="555.319" m="217.775" t="1.334"/>\r
+<eng-data cg="163." f="560.042" m="179.977" t="1.47"/>\r
+<eng-data cg="163." f="559.841" m="147.049" t="1.588"/>\r
+<eng-data cg="163." f="546.98" m="98.5088" t="1.764"/>\r
+<eng-data cg="163." f="516.838" m="56.8911" t="1.921"/>\r
+<eng-data cg="163." f="496.743" m="38.7066" t="1.993"/>\r
+<eng-data cg="163." f="499.154" m="30.7656" t="2.025"/>\r
+<eng-data cg="163." f="479.16" m="25.4025" t="2.047"/>\r
+<eng-data cg="163." f="414.354" m="16.7194" t="2.086"/>\r
+<eng-data cg="163." f="344.525" m="11.2356" t="2.115"/>\r
+<eng-data cg="163." f="252.29" m="7.36905" t="2.141"/>\r
+<eng-data cg="163." f="140.161" m="3.84859" t="2.177"/>\r
+<eng-data cg="163." f="82.78" m="1.84871" t="2.213"/>\r
+<eng-data cg="163." f="50.347" m="0.98623" t="2.239"/>\r
+<eng-data cg="163." f="27.861" m="0.362621" t="2.271"/>\r
+<eng-data cg="163." f="12.86" m="0.108951" t="2.296"/>\r
+<eng-data cg="163." f="0." m="0." t="2.33"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works J450 Super Tiger\r
-J450ST 54 326 0 0.5331 1.1964 AMW\r
-0.009 251.586\r
-0.016 376.074\r
-0.030 413.450\r
-0.051 430.832\r
-0.094 423.296\r
-0.162 413.149\r
-0.262 395.566\r
-0.402 420.182\r
-0.495 444.898\r
-0.805 504.078\r
-1.048 536.028\r
-1.223 550.597\r
-1.299 563.180\r
-1.334 555.319\r
-1.470 560.042\r
-1.588 559.841\r
-1.764 546.980\r
-1.921 516.838\r
-1.993 496.743\r
-2.025 499.154\r
-2.047 479.160\r
-2.086 414.354\r
-2.115 344.525\r
-2.141 252.290\r
-2.177 140.161\r
-2.213 82.780\r
-2.239 50.347\r
-2.271 27.861\r
-2.296 12.860\r
-2.330 0.000\r
+++ /dev/null
-;\r
-;AMW J480 RASP.ENG file made from NAR published data\r
-;File produced April 19, 2004\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-J480BB 54 326 100 0.556 1.2131 Animal_Motor_Works \r
-0.015 225.429\r
-0.041 348.18\r
-0.071 388.127\r
-0.194 422.453\r
-0.385 459.49\r
-0.699 502.347\r
-0.968 528.042\r
-1.2 536.573\r
-1.454 543.15\r
-1.674 533.763\r
-1.887 522.321\r
-2.044 519.41\r
-2.108 525.131\r
-2.164 528.042\r
-2.197 488.095\r
-2.25 419.543\r
-2.283 333.928\r
-2.328 231.15\r
-2.354 176.95\r
-2.392 111.309\r
-2.418 68.501\r
-2.436 37.106\r
-2.49 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="212.96" Itot="1161.14" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="466.323" burn-time="2.49" cgDiv="10" cgFix="1" cgStep="-1." code="J480BB" delays="1000" dia="54." exitDia="0." initWt="1213.1" len="326." mDiv="10" mFix="1" mStep="-1." massFrac="45.83" mfg="Animal Motor Works" peakThrust="543.15" propWt="556." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW J480 RASP.ENG file made from NAR published data\r
+File produced April 19, 2004\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="163." f="0." m="556." t="0."/>\r
+<eng-data cg="163." f="225.429" m="555.19" t="0.015"/>\r
+<eng-data cg="163." f="348.18" m="551.62" t="0.041"/>\r
+<eng-data cg="163." f="388.127" m="546.331" t="0.071"/>\r
+<eng-data cg="163." f="422.453" m="522.461" t="0.194"/>\r
+<eng-data cg="163." f="459.49" m="482.13" t="0.385"/>\r
+<eng-data cg="163." f="502.347" m="409.822" t="0.699"/>\r
+<eng-data cg="163." f="528.042" m="343.461" t="0.968"/>\r
+<eng-data cg="163." f="536.573" m="284.327" t="1.2"/>\r
+<eng-data cg="163." f="543.15" m="218.666" t="1.454"/>\r
+<eng-data cg="163." f="533.763" m="161.943" t="1.674"/>\r
+<eng-data cg="163." f="522.321" m="108.087" t="1.887"/>\r
+<eng-data cg="163." f="519.41" m="68.9294" t="2.044"/>\r
+<eng-data cg="163." f="525.131" m="52.9241" t="2.108"/>\r
+<eng-data cg="163." f="528.042" m="38.8037" t="2.164"/>\r
+<eng-data cg="163." f="488.095" m="30.7754" t="2.197"/>\r
+<eng-data cg="163." f="419.543" m="19.2582" t="2.25"/>\r
+<eng-data cg="163." f="333.928" m="13.3051" t="2.283"/>\r
+<eng-data cg="163." f="231.15" m="7.21708" t="2.328"/>\r
+<eng-data cg="163." f="176.95" m="4.6767" t="2.354"/>\r
+<eng-data cg="163." f="111.309" m="2.05414" t="2.392"/>\r
+<eng-data cg="163." f="68.501" m="0.934847" t="2.418"/>\r
+<eng-data cg="163." f="37.106" m="0.479729" t="2.436"/>\r
+<eng-data cg="163." f="0." m="0." t="2.49"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;J500ST entered by Tim Van Milligan\r
-;For RockSim - http://www.rocksim.com\r
-;Based on TRA Certification paperwork from 06-01-2002\r
-;Initial Mass from Jim Robinson at AMW\r
-;Not approved by TRA or AMW.\r
-J500ST 38 370 20 0.3265 0.744 Animal_Motor_Works \r
-0.006 444.822\r
-0.025 475.651\r
-0.04 418.397\r
-0.053 466.843\r
-0.059 409.589\r
-0.071 458.035\r
-0.077 409.589\r
-0.1 444.822\r
-0.127 506.481\r
-0.204 590.16\r
-0.25 644.992\r
-0.3 678.244\r
-0.34 709.073\r
-0.402 735.498\r
-0.445 766.327\r
-0.516 783.944\r
-0.6 787.335\r
-0.637 770.732\r
-0.68 744.306\r
-0.76 620.989\r
-0.859 475.651\r
-1.00464 303.888\r
-1.122 171.763\r
-1.227 52.8502\r
-1.3 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="204.22" Itot="653.892" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="502.994" burn-time="1.3" cgDiv="10" cgFix="1" cgStep="-1." code="J500ST" delays="20" dia="38." exitDia="0." initWt="744." len="370." mDiv="10" mFix="1" mStep="-1." massFrac="43.88" mfg="Animal Motor Works" peakThrust="787.335" propWt="326.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>J500ST entered by Tim Van Milligan\r
+For RockSim - http://www.rocksim.com\r
+Based on TRA Certification paperwork from 06-01-2002\r
+Initial Mass from Jim Robinson at AMW\r
+Not approved by TRA or AMW.\r
+</comments>\r
+<data>\r
+<eng-data cg="185." f="0." m="326.5" t="0."/>\r
+<eng-data cg="185." f="444.822" m="325.834" t="0.006"/>\r
+<eng-data cg="185." f="475.651" m="321.467" t="0.025"/>\r
+<eng-data cg="185." f="418.397" m="318.119" t="0.04"/>\r
+<eng-data cg="185." f="466.843" m="315.246" t="0.053"/>\r
+<eng-data cg="185." f="409.589" m="313.933" t="0.059"/>\r
+<eng-data cg="185." f="458.035" m="311.334" t="0.071"/>\r
+<eng-data cg="185." f="409.589" m="310.034" t="0.077"/>\r
+<eng-data cg="185." f="444.822" m="305.128" t="0.1"/>\r
+<eng-data cg="185." f="506.481" m="298.716" t="0.127"/>\r
+<eng-data cg="185." f="590.16" m="277.634" t="0.204"/>\r
+<eng-data cg="185." f="644.992" m="263.449" t="0.25"/>\r
+<eng-data cg="185." f="678.244" m="246.931" t="0.3"/>\r
+<eng-data cg="185." f="709.073" m="233.077" t="0.34"/>\r
+<eng-data cg="185." f="735.498" m="210.717" t="0.402"/>\r
+<eng-data cg="185." f="766.327" m="194.594" t="0.445"/>\r
+<eng-data cg="185." f="783.944" m="167.114" t="0.516"/>\r
+<eng-data cg="185." f="787.335" m="134.163" t="0.6"/>\r
+<eng-data cg="185." f="770.732" m="119.77" t="0.637"/>\r
+<eng-data cg="185." f="744.306" m="103.506" t="0.68"/>\r
+<eng-data cg="185." f="620.989" m="76.237" t="0.76"/>\r
+<eng-data cg="185." f="475.651" m="49.1321" t="0.859"/>\r
+<eng-data cg="185." f="303.888" m="20.7878" t="1.00464"/>\r
+<eng-data cg="185." f="171.763" m="6.85126" t="1.122"/>\r
+<eng-data cg="185." f="52.8502" m="0.963201" t="1.227"/>\r
+<eng-data cg="185." f="0." m="0." t="1.3"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;AMW K1000 RASP.ENG file made from NAR published data\r
-;File produced April 19, 2004\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-K1000SK 54 728 100 1.297 2.556 Animal_Motor_Works \r
-0.019 1155.06\r
-0.045 1426.12\r
-0.094 1248.23\r
-0.161 1112.99\r
-0.239 1128.02\r
-0.343 1113.99\r
-0.377 1149.05\r
-0.44 1121\r
-0.544 1221.18\r
-0.633 1178.11\r
-0.674 1221.18\r
-0.737 1193.13\r
-0.883 1200.14\r
-1.009 1194.13\r
-1.057 1236.21\r
-1.188 1137.03\r
-1.299 1145.05\r
-1.396 1087.94\r
-1.516 954.104\r
-1.631 855.228\r
-1.717 827.077\r
-1.777 650.061\r
-1.848 465.932\r
-1.93 303.141\r
-2.023 147.463\r
-2.083 83.879\r
-2.132 41.484\r
-2.18 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="163.34" Itot="2077.51" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="952.987" burn-time="2.18" cgDiv="10" cgFix="1" cgStep="-1." code="K1000SK" delays="1000" dia="54." exitDia="0." initWt="2556." len="728." mDiv="10" mFix="1" mStep="-1." massFrac="50.74" mfg="Animal Motor Works" peakThrust="1426.12" propWt="1297." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW K1000 RASP.ENG file made from NAR published data\r
+File produced April 19, 2004\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="364." f="0." m="1297." t="0."/>\r
+<eng-data cg="364." f="1155.06" m="1290.15" t="0.019"/>\r
+<eng-data cg="364." f="1426.12" m="1269.2" t="0.045"/>\r
+<eng-data cg="364." f="1248.23" m="1228.3" t="0.094"/>\r
+<eng-data cg="364." f="1112.99" m="1178.91" t="0.161"/>\r
+<eng-data cg="364." f="1128.02" m="1124.35" t="0.239"/>\r
+<eng-data cg="364." f="1113.99" m="1051.56" t="0.343"/>\r
+<eng-data cg="364." f="1149.05" m="1027.55" t="0.377"/>\r
+<eng-data cg="364." f="1121." m="982.904" t="0.44"/>\r
+<eng-data cg="364." f="1221.18" m="906.868" t="0.544"/>\r
+<eng-data cg="364." f="1178.11" m="840.212" t="0.633"/>\r
+<eng-data cg="364." f="1221.18" m="809.506" t="0.674"/>\r
+<eng-data cg="364." f="1193.13" m="762.027" t="0.737"/>\r
+<eng-data cg="364." f="1200.14" m="652.955" t="0.883"/>\r
+<eng-data cg="364." f="1194.13" m="558.786" t="1.009"/>\r
+<eng-data cg="364." f="1236.21" m="522.371" t="1.057"/>\r
+<eng-data cg="364." f="1137.03" m="425.325" t="1.188"/>\r
+<eng-data cg="364." f="1145.05" m="346.253" t="1.299"/>\r
+<eng-data cg="364." f="1087.94" m="278.641" t="1.396"/>\r
+<eng-data cg="364." f="954.104" m="202.15" t="1.516"/>\r
+<eng-data cg="364." f="855.228" m="137.199" t="1.631"/>\r
+<eng-data cg="364." f="827.077" m="92.0376" t="1.717"/>\r
+<eng-data cg="364." f="650.061" m="64.3721" t="1.777"/>\r
+<eng-data cg="364." f="465.932" m="39.6386" t="1.848"/>\r
+<eng-data cg="364." f="303.141" m="19.953" t="1.93"/>\r
+<eng-data cg="364." f="147.463" m="6.87189" t="2.023"/>\r
+<eng-data cg="364." f="83.879" m="2.53905" t="2.083"/>\r
+<eng-data cg="364." f="41.484" m="0.621567" t="2.132"/>\r
+<eng-data cg="364." f="0." m="0." t="2.18"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works K1075 RASP.ENG file made from NAR data\r
-;File produced Feb 22, 2003\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-K1075GG 54 726 100 1.3999 2.6658 Animal_Motor_Works \r
-0.009 672.664\r
-0.015 963.511\r
-0.022 860.518\r
-0.047 987.857\r
-0.075 975.835\r
-0.106 921.332\r
-0.215 958.001\r
-0.529 1092.05\r
-0.878 1220.29\r
-1.077 1269.39\r
-1.158 1311.47\r
-1.235 1293.43\r
-1.448 1330.5\r
-1.577 1318.48\r
-1.672 1319.48\r
-1.721 1337.52\r
-1.759 1337.52\r
-1.805 1337.52\r
-1.829 1331.5\r
-1.856 1384.67\r
-1.889 1277.4\r
-1.906 1216.29\r
-1.938 1052.98\r
-1.96 871.338\r
-1.988 659.239\r
-2.027 453.352\r
-2.062 301.967\r
-2.115 138.46\r
-2.168 41.608\r
-2.2 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="174.27" Itot="2392.45" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1087.48" burn-time="2.2" cgDiv="10" cgFix="1" cgStep="-1." code="K1075GG" delays="1000" dia="54." exitDia="0." initWt="2665.8" len="726." mDiv="10" mFix="1" mStep="-1." massFrac="52.51" mfg="Animal Motor Works" peakThrust="1384.67" propWt="1399.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Animal Motor Works K1075 RASP.ENG file made from NAR data\r
+File produced Feb 22, 2003\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="363." f="0." m="1399.9" t="0."/>\r
+<eng-data cg="363." f="672.664" m="1398.13" t="0.009"/>\r
+<eng-data cg="363." f="963.511" m="1395.26" t="0.015"/>\r
+<eng-data cg="363." f="860.518" m="1391.52" t="0.022"/>\r
+<eng-data cg="363." f="987.857" m="1378." t="0.047"/>\r
+<eng-data cg="363." f="975.835" m="1361.92" t="0.075"/>\r
+<eng-data cg="363." f="921.332" m="1344.71" t="0.106"/>\r
+<eng-data cg="363." f="958.001" m="1284.78" t="0.215"/>\r
+<eng-data cg="363." f="1092.05" m="1096.45" t="0.529"/>\r
+<eng-data cg="363." f="1220.29" m="860.344" t="0.878"/>\r
+<eng-data cg="363." f="1269.39" m="715.393" t="1.077"/>\r
+<eng-data cg="363." f="1311.47" m="654.232" t="1.158"/>\r
+<eng-data cg="363." f="1293.43" m="595.55" t="1.235"/>\r
+<eng-data cg="363." f="1330.5" m="432.035" t="1.448"/>\r
+<eng-data cg="363." f="1318.48" m="332.06" t="1.577"/>\r
+<eng-data cg="363." f="1319.48" m="258.741" t="1.672"/>\r
+<eng-data cg="363." f="1337.52" m="220.651" t="1.721"/>\r
+<eng-data cg="363." f="1337.52" m="190.911" t="1.759"/>\r
+<eng-data cg="363." f="1337.52" m="154.91" t="1.805"/>\r
+<eng-data cg="363." f="1331.5" m="136.169" t="1.829"/>\r
+<eng-data cg="363." f="1384.67" m="114.714" t="1.856"/>\r
+<eng-data cg="363." f="1277.4" m="89.0121" t="1.889"/>\r
+<eng-data cg="363." f="1216.29" m="76.6094" t="1.906"/>\r
+<eng-data cg="363." f="1052.98" m="55.3642" t="1.938"/>\r
+<eng-data cg="363." f="871.338" m="42.9784" t="1.96"/>\r
+<eng-data cg="363." f="659.239" m="30.4401" t="1.988"/>\r
+<eng-data cg="363." f="453.352" m="17.7453" t="2.027"/>\r
+<eng-data cg="363." f="301.967" m="10.011" t="2.062"/>\r
+<eng-data cg="363." f="138.46" m="3.18168" t="2.115"/>\r
+<eng-data cg="363." f="41.608" m="0.38954" t="2.168"/>\r
+<eng-data cg="363." f="0." m="0." t="2.2"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;AMW K365RR RASP.ENG file made from NAR published data\r
-;File produced April 19, 2004\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-K365RR 75 111 100 0.946 2.3456 Animal_Motor_Works \r
-0.049 138.157\r
-0.068 381.241\r
-0.084 454.75\r
-0.106 481.536\r
-0.164 488.182\r
-0.291 514.867\r
-0.435 545.982\r
-0.666 561.49\r
-0.868 565.73\r
-1.082 565.518\r
-1.296 550.111\r
-1.591 529.871\r
-1.805 509.731\r
-1.828 536.517\r
-1.886 498.554\r
-2.124 467.237\r
-2.501 411.35\r
-2.924 328.677\r
-3.296 241.573\r
-3.638 172.293\r
-3.969 100.798\r
-4.195 56.098\r
-4.265 51.607\r
-4.346 35.959\r
-4.433 15.859\r
-4.51 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="180.58" Itot="1675.27" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="371.456" burn-time="4.51" cgDiv="10" cgFix="1" cgStep="-1." code="K365RR" delays="1000" dia="75." exitDia="0." initWt="2345.6" len="111." mDiv="10" mFix="1" mStep="-1." massFrac="40.33" mfg="Animal Motor Works" peakThrust="565.73" propWt="946." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW K365RR RASP.ENG file made from NAR published data\r
+File produced April 19, 2004\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="55.5" f="0." m="946." t="0."/>\r
+<eng-data cg="55.5" f="138.157" m="944.089" t="0.049"/>\r
+<eng-data cg="55.5" f="381.241" m="941.302" t="0.068"/>\r
+<eng-data cg="55.5" f="454.75" m="937.526" t="0.084"/>\r
+<eng-data cg="55.5" f="481.536" m="931.71" t="0.106"/>\r
+<eng-data cg="55.5" f="488.182" m="915.83" t="0.164"/>\r
+<eng-data cg="55.5" f="514.867" m="879.863" t="0.291"/>\r
+<eng-data cg="55.5" f="545.982" m="836.732" t="0.435"/>\r
+<eng-data cg="55.5" f="561.49" m="764.501" t="0.666"/>\r
+<eng-data cg="55.5" f="565.73" m="700.212" t="0.868"/>\r
+<eng-data cg="55.5" f="565.518" m="631.86" t="1.082"/>\r
+<eng-data cg="55.5" f="550.111" m="564.452" t="1.296"/>\r
+<eng-data cg="55.5" f="529.871" m="474.499" t="1.591"/>\r
+<eng-data cg="55.5" f="509.731" m="411.685" t="1.805"/>\r
+<eng-data cg="55.5" f="536.517" m="404.891" t="1.828"/>\r
+<eng-data cg="55.5" f="498.554" m="387.941" t="1.886"/>\r
+<eng-data cg="55.5" f="467.237" m="323.042" t="2.124"/>\r
+<eng-data cg="55.5" f="411.35" m="229.522" t="2.501"/>\r
+<eng-data cg="55.5" f="328.677" m="141.14" t="2.924"/>\r
+<eng-data cg="55.5" f="241.573" m="81.2457" t="3.296"/>\r
+<eng-data cg="55.5" f="172.293" m="41.2823" t="3.638"/>\r
+<eng-data cg="55.5" f="100.798" m="15.7604" t="3.969"/>\r
+<eng-data cg="55.5" f="56.098" m="5.74893" t="4.195"/>\r
+<eng-data cg="55.5" f="51.607" m="3.62025" t="4.265"/>\r
+<eng-data cg="55.5" f="35.959" m="1.61763" t="4.346"/>\r
+<eng-data cg="55.5" f="15.859" m="0.344781" t="4.433"/>\r
+<eng-data cg="55.5" f="0." m="0." t="4.51"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;AMW K450BB RASP.ENG file made from NAR published data\r
-;File produced Aug 19, 2003\r
-;This file my be used or given away. All I ask is that this header\r
-;is maintained to give credit to NAR S&T. Thank you, Jack Kane.\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-K450BB 75 302 100 0.8816 2.8349 Animal_Motor_Works \r
-0.03 78.903\r
-0.045 227.9\r
-0.064 449.955\r
-0.069 508.417\r
-0.094 555.187\r
-0.151 563.956\r
-0.362 625.442\r
-0.562 651.85\r
-0.825 660.62\r
-1.134 652.254\r
-1.453 626.147\r
-1.793 594.296\r
-2.113 538.958\r
-2.458 469.106\r
-2.798 384.538\r
-3.165 276.686\r
-3.201 279.609\r
-3.325 232.94\r
-3.51 171.757\r
-3.732 107.65\r
-3.861 58.018\r
-3.959 40.55\r
-4.036 20.149\r
-4.11 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="213.76" Itot="1848.03" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="449.643" burn-time="4.11" cgDiv="10" cgFix="1" cgStep="-1." code="K450BB" delays="1000" dia="75." exitDia="0." initWt="2834.9" len="302." mDiv="10" mFix="1" mStep="-1." massFrac="31.1" mfg="Animal Motor Works" peakThrust="660.62" propWt="881.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments><![CDATA[AMW K450BB RASP.ENG file made from NAR published data\r
+File produced Aug 19, 2003\r
+This file my be used or given away. All I ask is that this header\r
+is maintained to give credit to NAR S&T. Thank you, Jack Kane.\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+]]></comments>\r
+<data>\r
+<eng-data cg="151." f="0." m="881.6" t="0."/>\r
+<eng-data cg="151." f="78.903" m="881.035" t="0.03"/>\r
+<eng-data cg="151." f="227.9" m="879.938" t="0.045"/>\r
+<eng-data cg="151." f="449.955" m="876.866" t="0.064"/>\r
+<eng-data cg="151." f="508.417" m="875.723" t="0.069"/>\r
+<eng-data cg="151." f="555.187" m="869.38" t="0.094"/>\r
+<eng-data cg="151." f="563.956" m="854.165" t="0.151"/>\r
+<eng-data cg="151." f="625.442" m="794.304" t="0.362"/>\r
+<eng-data cg="151." f="651.85" m="733.371" t="0.562"/>\r
+<eng-data cg="151." f="660.62" m="651.038" t="0.825"/>\r
+<eng-data cg="151." f="652.254" m="554.274" t="1.134"/>\r
+<eng-data cg="151." f="626.147" m="457.001" t="1.453"/>\r
+<eng-data cg="151." f="594.296" m="358.026" t="1.793"/>\r
+<eng-data cg="151." f="538.958" m="271.527" t="2.113"/>\r
+<eng-data cg="151." f="469.106" m="188.573" t="2.458"/>\r
+<eng-data cg="151." f="384.538" m="119.344" t="2.798"/>\r
+<eng-data cg="151." f="276.686" m="61.4618" t="3.165"/>\r
+<eng-data cg="151." f="279.609" m="56.6849" t="3.201"/>\r
+<eng-data cg="151." f="232.94" m="41.5253" t="3.325"/>\r
+<eng-data cg="151." f="171.757" m="23.6673" t="3.51"/>\r
+<eng-data cg="151." f="107.65" m="8.87205" t="3.732"/>\r
+<eng-data cg="151." f="58.018" m="3.77452" t="3.861"/>\r
+<eng-data cg="151." f="40.55" m="1.47046" t="3.959"/>\r
+<eng-data cg="151." f="20.149" m="0.355645" t="4.036"/>\r
+<eng-data cg="151." f="0." m="0." t="4.11"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;AMW K470ST RASP.ENG file made from Tripoli published data\r
-;File produced May 15, 2004\r
-;This file my be used or given away. All I ask is that this header\r
-;is maintained to give credit to the people who produced the data.\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-K470ST 75 302 100 0.826 2.779 Animal_Motor_Works \r
-0.028 699.309\r
-0.039 799.337\r
-0.09 765.845\r
-0.157 770.311\r
-0.258 785.941\r
-0.41 804\r
-0.572 794.425\r
-0.707 794.425\r
-0.886 792.192\r
-0.998 783.261\r
-1.15 752.002\r
-1.318 709.579\r
-1.447 655.992\r
-1.593 595.707\r
-1.728 522.025\r
-1.885 444.101\r
-2.092 354.923\r
-2.356 270.167\r
-2.664 187.554\r
-2.945 131.734\r
-3.27 78.058\r
-3.433 55.686\r
-3.478 48.987\r
-3.556 28.909\r
-3.7 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="207.28" Itot="1679." Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="453.784" burn-time="3.7" cgDiv="10" cgFix="1" cgStep="-1." code="K470ST" delays="1000" dia="75." exitDia="0." initWt="2779." len="302." mDiv="10" mFix="1" mStep="-1." massFrac="29.72" mfg="Animal Motor Works" peakThrust="804." propWt="826." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW K470ST RASP.ENG file made from Tripoli published data\r
+File produced May 15, 2004\r
+This file my be used or given away. All I ask is that this header\r
+is maintained to give credit to the people who produced the data.\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="151." f="0." m="826." t="0."/>\r
+<eng-data cg="151." f="699.309" m="821.184" t="0.028"/>\r
+<eng-data cg="151." f="799.337" m="817.129" t="0.039"/>\r
+<eng-data cg="151." f="765.845" m="797.493" t="0.09"/>\r
+<eng-data cg="151." f="770.311" m="772.177" t="0.157"/>\r
+<eng-data cg="151." f="785.941" m="733.513" t="0.258"/>\r
+<eng-data cg="151." f="804." m="674.067" t="0.41"/>\r
+<eng-data cg="151." f="794.425" m="610.372" t="0.572"/>\r
+<eng-data cg="151." f="794.425" m="557.61" t="0.707"/>\r
+<eng-data cg="151." f="792.192" m="487.751" t="0.886"/>\r
+<eng-data cg="151." f="783.261" m="444.348" t="0.998"/>\r
+<eng-data cg="151." f="752.002" m="386.946" t="1.15"/>\r
+<eng-data cg="151." f="709.579" m="326.547" t="1.318"/>\r
+<eng-data cg="151." f="655.992" m="283.215" t="1.447"/>\r
+<eng-data cg="151." f="595.707" m="238.263" t="1.593"/>\r
+<eng-data cg="151." f="522.025" m="201.146" t="1.728"/>\r
+<eng-data cg="151." f="444.101" m="163.835" t="1.885"/>\r
+<eng-data cg="151." f="354.923" m="123.151" t="2.092"/>\r
+<eng-data cg="151." f="270.167" m="82.5581" t="2.356"/>\r
+<eng-data cg="151." f="187.554" m="47.8804" t="2.664"/>\r
+<eng-data cg="151." f="131.734" m="25.8111" t="2.945"/>\r
+<eng-data cg="151." f="78.058" m="9.0396" t="3.27"/>\r
+<eng-data cg="151." f="55.686" m="3.67717" t="3.433"/>\r
+<eng-data cg="151." f="48.987" m="2.51853" t="3.478"/>\r
+<eng-data cg="151." f="28.909" m="1.02399" t="3.556"/>\r
+<eng-data cg="151." f="0." m="0." t="3.7"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works K475 RASP.ENG file made from NAR data\r
-;File produced Feb 22, 2003\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-K475WW 54 403 100 0.7286 1.4925 Animal_Motor_Works \r
-0.022 127.831\r
-0.041 386.016\r
-0.063 548.326\r
-0.096 521.308\r
-0.134 499.129\r
-0.18 486.83\r
-0.285 486.83\r
-0.478 501.649\r
-0.731 523.727\r
-1.096 553.266\r
-1.433 577.962\r
-1.601 588.29\r
-1.756 582.704\r
-1.895 580.284\r
-1.958 575.344\r
-2.063 550.746\r
-2.209 518.788\r
-2.344 477.051\r
-2.495 417.974\r
-2.561 354.058\r
-2.582 334.399\r
-2.599 331.98\r
-2.62 297.501\r
-2.67 226.226\r
-2.707 157.37\r
-2.74 98.353\r
-2.799 49.176\r
-2.853 17.208\r
-2.94 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="195.08" Itot="1393.88" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="474.108" burn-time="2.94" cgDiv="10" cgFix="1" cgStep="-1." code="K475WW" delays="1000" dia="54." exitDia="0." initWt="1492.5" len="403." mDiv="10" mFix="1" mStep="-1." massFrac="48.82" mfg="Animal Motor Works" peakThrust="588.29" propWt="728.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Animal Motor Works K475 RASP.ENG file made from NAR data\r
+File produced Feb 22, 2003\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="201.5" f="0." m="728.6" t="0."/>\r
+<eng-data cg="201.5" f="127.831" m="727.865" t="0.022"/>\r
+<eng-data cg="201.5" f="386.016" m="725.313" t="0.041"/>\r
+<eng-data cg="201.5" f="548.326" m="719.941" t="0.063"/>\r
+<eng-data cg="201.5" f="521.308" m="710.716" t="0.096"/>\r
+<eng-data cg="201.5" f="499.129" m="700.581" t="0.134"/>\r
+<eng-data cg="201.5" f="486.83" m="688.727" t="0.18"/>\r
+<eng-data cg="201.5" f="486.83" m="662.008" t="0.285"/>\r
+<eng-data cg="201.5" f="501.649" m="612.147" t="0.478"/>\r
+<eng-data cg="201.5" f="523.727" m="544.346" t="0.731"/>\r
+<eng-data cg="201.5" f="553.266" m="441.605" t="1.096"/>\r
+<eng-data cg="201.5" f="577.962" m="341.97" t="1.433"/>\r
+<eng-data cg="201.5" f="588.29" m="290.762" t="1.601"/>\r
+<eng-data cg="201.5" f="582.704" m="243.324" t="1.756"/>\r
+<eng-data cg="201.5" f="580.284" m="201.074" t="1.895"/>\r
+<eng-data cg="201.5" f="575.344" m="182.046" t="1.958"/>\r
+<eng-data cg="201.5" f="550.746" m="151.144" t="2.063"/>\r
+<eng-data cg="201.5" f="518.788" m="110.332" t="2.209"/>\r
+<eng-data cg="201.5" f="477.051" m="75.1958" t="2.344"/>\r
+<eng-data cg="201.5" f="417.974" m="39.8736" t="2.495"/>\r
+<eng-data cg="201.5" f="354.058" m="26.5564" t="2.561"/>\r
+<eng-data cg="201.5" f="334.399" m="22.7778" t="2.582"/>\r
+<eng-data cg="201.5" f="331.98" m="19.817" t="2.599"/>\r
+<eng-data cg="201.5" f="297.501" m="16.3621" t="2.62"/>\r
+<eng-data cg="201.5" f="226.226" m="9.5181" t="2.67"/>\r
+<eng-data cg="201.5" f="157.37" m="5.80864" t="2.707"/>\r
+<eng-data cg="201.5" f="98.353" m="3.60308" t="2.74"/>\r
+<eng-data cg="201.5" f="49.176" m="1.32817" t="2.799"/>\r
+<eng-data cg="201.5" f="17.208" m="0.391277" t="2.853"/>\r
+<eng-data cg="201.5" f="0." m="0." t="2.94"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Animal" code="K500SK" Type="reloadable" dia="75." len="368." initWt="2713."\r
+propWt="1123.5" delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="455.234" peakThrust="841.432" throatDia="0." exitDia="0."\r
+Itot="1796.35" burn-time="3.95" massFrac="41.41" Isp="163.04" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Entered by Tim Van Milligan. Used John Coker's ThrustCurve Tracer software and\r
+data from NAR certification dated May 7, 2007\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="1123.5" cg="184."/>\r
+<eng-data t="0.018" f="194.373" m="1122.41" cg="184."/>\r
+<eng-data t="0.031" f="207.161" m="1120.77" cg="184."/>\r
+<eng-data t="0.036" f="268.542" m="1120.03" cg="184."/>\r
+<eng-data t="0.103" f="319.693" m="1107.71" cg="184."/>\r
+<eng-data t="0.138" f="322.251" m="1100.68" cg="184."/>\r
+<eng-data t="0.17" f="314.578" m="1094.31" cg="184."/>\r
+<eng-data t="0.67" f="309.463" m="996.732" cg="184."/>\r
+<eng-data t="0.692" f="322.251" m="992.386" cg="184."/>\r
+<eng-data t="0.902" f="319.693" m="950.229" cg="184."/>\r
+<eng-data t="0.929" f="332.481" m="944.723" cg="184."/>\r
+<eng-data t="1.263" f="355.499" m="872.865" cg="184."/>\r
+<eng-data t="1.585" f="383.632" m="798.438" cg="184."/>\r
+<eng-data t="1.969" f="411.765" m="702.924" cg="184."/>\r
+<eng-data t="2.112" f="416.88" m="665.869" cg="184."/>\r
+<eng-data t="2.272" f="447.57" m="622.616" cg="184."/>\r
+<eng-data t="2.415" f="488.491" m="580.757" cg="184."/>\r
+<eng-data t="2.46" f="485.934" m="567.044" cg="184."/>\r
+<eng-data t="2.634" f="534.527" m="511.518" cg="184."/>\r
+<eng-data t="2.83" f="618.926" m="440.82" cg="184."/>\r
+<eng-data t="3.018" f="710.997" m="362.633" cg="184."/>\r
+<eng-data t="3.143" f="767.263" m="304.849" cg="184."/>\r
+<eng-data t="3.228" f="815.857" m="262.768" cg="184."/>\r
+<eng-data t="3.339" f="841.432" m="205.241" cg="184."/>\r
+<eng-data t="3.402" f="826.087" m="172.389" cg="184."/>\r
+<eng-data t="3.504" f="785.166" m="120.994" cg="184."/>\r
+<eng-data t="3.585" f="718.67" m="82.902" cg="184."/>\r
+<eng-data t="3.661" f="631.714" m="50.8081" cg="184."/>\r
+<eng-data t="3.728" f="519.182" m="26.6945" cg="184."/>\r
+<eng-data t="3.772" f="365.729" m="14.5185" cg="184."/>\r
+<eng-data t="3.826" f="181.586" m="5.27619" cg="184."/>\r
+<eng-data t="3.862" f="99.744" m="2.10903" cg="184."/>\r
+<eng-data t="3.893" f="43.478" m="0.720604" cg="184."/>\r
+<eng-data t="3.946" f="0." m="0." cg="184."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works 54-1400\r
-;AMW K530GG RASP.ENG file made from NAR data\r
-;File produced Feb 25, 2003\r
-;This file my be used or given away. All I ask is that this header\r
-;is maintained to give credit to NAR S&T. Thank you, Jack Kane\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-K530GG 54 403 1000 0.7967 1.616 Animal_Motor_Works \r
-0.013 129.764\r
-0.054 171.852\r
-0.096 284.122\r
-0.138 392.892\r
-0.171 455.975\r
-0.217 501.662\r
-0.238 498.063\r
-0.326 508.66\r
-0.542 564.745\r
-0.755 613.831\r
-1.01 645.423\r
-1.17 657.23\r
-1.273 648.922\r
-1.51 638.425\r
-1.656 634.925\r
-1.702 606.833\r
-1.803 606.833\r
-1.857 585.839\r
-1.936 589.338\r
-1.974 575.242\r
-2.015 589.338\r
-2.04 564.745\r
-2.132 536.652\r
-2.207 540.251\r
-2.291 522.656\r
-2.357 487.566\r
-2.42 375.297\r
-2.478 242.033\r
-2.529 140.361\r
-2.583 66.651\r
-2.66 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="179.39" Itot="1401.55" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="526.897" burn-time="2.66" cgDiv="10" cgFix="1" cgStep="-1." code="K530GG" delays="1000" dia="54." exitDia="0." initWt="1616." len="403." mDiv="10" mFix="1" mStep="-1." massFrac="49.3" mfg="Animal Motor Works" peakThrust="657.23" propWt="796.7" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments><![CDATA[Animal Motor Works 54-1400\r
+AMW K530GG RASP.ENG file made from NAR data\r
+File produced Feb 25, 2003\r
+This file my be used or given away. All I ask is that this header\r
+is maintained to give credit to NAR S&T. Thank you, Jack Kane\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+]]></comments>\r
+<data>\r
+<eng-data cg="201.5" f="0." m="796.7" t="0."/>\r
+<eng-data cg="201.5" f="129.764" m="796.221" t="0.013"/>\r
+<eng-data cg="201.5" f="171.852" m="792.706" t="0.054"/>\r
+<eng-data cg="201.5" f="284.122" m="787.263" t="0.096"/>\r
+<eng-data cg="201.5" f="392.892" m="779.181" t="0.138"/>\r
+<eng-data cg="201.5" f="455.975" m="771.219" t="0.171"/>\r
+<eng-data cg="201.5" f="501.662" m="758.699" t="0.217"/>\r
+<eng-data cg="201.5" f="498.063" m="752.732" t="0.238"/>\r
+<eng-data cg="201.5" f="508.66" m="727.552" t="0.326"/>\r
+<eng-data cg="201.5" f="564.745" m="661.654" t="0.542"/>\r
+<eng-data cg="201.5" f="613.831" m="590.303" t="0.755"/>\r
+<eng-data cg="201.5" f="645.423" m="499.037" t="1.01"/>\r
+<eng-data cg="201.5" f="657.23" m="439.798" t="1.17"/>\r
+<eng-data cg="201.5" f="648.922" m="401.561" t="1.273"/>\r
+<eng-data cg="201.5" f="638.425" m="314.844" t="1.51"/>\r
+<eng-data cg="201.5" f="634.925" m="262.005" t="1.656"/>\r
+<eng-data cg="201.5" f="606.833" m="245.77" t="1.702"/>\r
+<eng-data cg="201.5" f="606.833" m="210.93" t="1.803"/>\r
+<eng-data cg="201.5" f="585.839" m="192.625" t="1.857"/>\r
+<eng-data cg="201.5" f="589.338" m="166.238" t="1.936"/>\r
+<eng-data cg="201.5" f="575.242" m="153.66" t="1.974"/>\r
+<eng-data cg="201.5" f="589.338" m="140.089" t="2.015"/>\r
+<eng-data cg="201.5" f="564.745" m="131.889" t="2.04"/>\r
+<eng-data cg="201.5" f="536.652" m="103.089" t="2.132"/>\r
+<eng-data cg="201.5" f="540.251" m="80.1328" t="2.207"/>\r
+<eng-data cg="201.5" f="522.656" m="54.7562" t="2.291"/>\r
+<eng-data cg="201.5" f="487.566" m="35.8058" t="2.357"/>\r
+<eng-data cg="201.5" f="375.297" m="20.3554" t="2.42"/>\r
+<eng-data cg="201.5" f="242.033" m="10.1788" t="2.478"/>\r
+<eng-data cg="201.5" f="140.361" m="4.63588" t="2.529"/>\r
+<eng-data cg="201.5" f="66.651" m="1.45866" t="2.583"/>\r
+<eng-data cg="201.5" f="0." m="0." t="2.66"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;Animal Motor Works 54-1750 K555 skidmark\r
-;File provide by Joel Rogers of AMW\r
-K555SK 54 492 0 0.8707 1.7343 AMW\r
-0.063 507.328\r
-0.144 535.181\r
-0.226 559.826\r
-0.308 585.793\r
-0.389 607.239\r
-0.471 629.034\r
-0.553 664.586\r
-0.634 683.688\r
-0.716 697.625\r
-0.798 719.618\r
-0.879 756.521\r
-0.961 777.700\r
-1.043 789.004\r
-1.124 797.934\r
-1.206 801.689\r
-1.288 804.331\r
-1.369 799.414\r
-1.451 768.014\r
-1.533 704.469\r
-1.614 641.709\r
-1.696 568.727\r
-1.778 481.013\r
-1.859 401.614\r
-1.941 333.897\r
-2.023 277.226\r
-2.104 205.009\r
-2.186 129.425\r
-2.268 73.717\r
-2.349 22.380\r
-2.368 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Animal Motor Works" code="K555SK" Type="reloadable" dia="54." len="492."\r
+initWt="1737." propWt="878.4" delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="560.673" peakThrust="936.468" throatDia="0." exitDia="0."\r
+Itot="1309.73" burn-time="2.34" massFrac="50.57" Isp="152.04" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>AMW K555 RASP.ENG file from Robert at AMW.</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="878.4" cg="246."/>\r
+ <eng-data t="0.061" f="508.351" m="868.001" cg="246."/>\r
+ <eng-data t="0.141" f="538.032" m="839.93" cg="246."/>\r
+ <eng-data t="0.222" f="573.058" m="809.751" cg="246."/>\r
+ <eng-data t="0.302" f="604.249" m="778.167" cg="246."/>\r
+ <eng-data t="0.383" f="631.13" m="744.612" cg="246."/>\r
+ <eng-data t="0.463" f="666.503" m="709.8" cg="246."/>\r
+ <eng-data t="0.544" f="696.284" m="672.784" cg="246."/>\r
+ <eng-data t="0.624" f="741.988" m="634.2" cg="246."/>\r
+ <eng-data t="0.705" f="787.186" m="592.664" cg="246."/>\r
+ <eng-data t="0.786" f="832.036" m="548.682" cg="246."/>\r
+ <eng-data t="0.866" f="869.416" m="503.038" cg="246."/>\r
+ <eng-data t="0.947" f="880.989" m="455.493" cg="246."/>\r
+ <eng-data t="1.027" f="912.349" m="407.383" cg="246."/>\r
+ <eng-data t="1.108" f="933.915" m="357.235" cg="246."/>\r
+ <eng-data t="1.188" f="936.468" m="307.058" cg="246."/>\r
+ <eng-data t="1.269" f="880.77" m="257.698" cg="246."/>\r
+ <eng-data t="1.349" f="784.951" m="213.012" cg="246."/>\r
+ <eng-data t="1.43" f="679.973" m="173.222" cg="246."/>\r
+ <eng-data t="1.511" f="572.224" m="139.209" cg="246."/>\r
+ <eng-data t="1.591" f="482.275" m="110.92" cg="246."/>\r
+ <eng-data t="1.672" f="407.793" m="86.7442" cg="246."/>\r
+ <eng-data t="1.752" f="347.675" m="66.4774" cg="246."/>\r
+ <eng-data t="1.833" f="286.395" m="49.2547" cg="246."/>\r
+ <eng-data t="1.913" f="235.942" m="35.242" cg="246."/>\r
+ <eng-data t="1.994" f="189.94" m="23.6742" cg="246."/>\r
+ <eng-data t="2.074" f="145.318" m="14.6802" cg="246."/>\r
+ <eng-data t="2.155" f="107.471" m="7.81394" cg="246."/>\r
+ <eng-data t="2.236" f="70.697" m="2.97451" cg="246."/>\r
+ <eng-data t="2.316" f="32.145" m="0.215587" cg="246."/>\r
+ <eng-data t="2.336" f="0." m="0." cg="246."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;AMW K560 RASP.ENG file made from NAR published data\r
-;File produced April 19, 2004\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-K560RR 54 430 100 0.75 1.5866 Animal_Motor_Works \r
-0.023 229.13\r
-0.046 415.135\r
-0.059 485.264\r
-0.078 512.268\r
-0.106 525.67\r
-0.154 523.05\r
-0.211 528.39\r
-0.261 536.451\r
-0.369 560.734\r
-0.511 587.738\r
-0.657 603.86\r
-0.77 612.022\r
-1.096 625.75\r
-1.358 620.083\r
-1.627 612.022\r
-1.839 603.86\r
-2.057 590.459\r
-2.218 598.52\r
-2.335 609.301\r
-2.385 601.24\r
-2.407 585.018\r
-2.426 533.831\r
-2.467 385.511\r
-2.507 283.037\r
-2.542 164.441\r
-2.576 67.399\r
-2.595 29.653\r
-2.62 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="200.34" Itot="1473.47" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="562.394" burn-time="2.62" cgDiv="10" cgFix="1" cgStep="-1." code="K560RR" delays="1000" dia="54." exitDia="0." initWt="1586.6" len="430." mDiv="10" mFix="1" mStep="-1." massFrac="47.27" mfg="Animal Motor Works" peakThrust="625.75" propWt="750." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW K560 RASP.ENG file made from NAR published data\r
+File produced April 19, 2004\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="215." f="0." m="750." t="0."/>\r
+<eng-data cg="215." f="229.13" m="748.659" t="0.023"/>\r
+<eng-data cg="215." f="415.135" m="744.888" t="0.046"/>\r
+<eng-data cg="215." f="485.264" m="741.909" t="0.059"/>\r
+<eng-data cg="215." f="512.268" m="737.085" t="0.078"/>\r
+<eng-data cg="215." f="525.67" m="729.689" t="0.106"/>\r
+<eng-data cg="215." f="523.05" m="716.877" t="0.154"/>\r
+<eng-data cg="215." f="528.39" m="701.625" t="0.211"/>\r
+<eng-data cg="215." f="536.451" m="688.074" t="0.261"/>\r
+<eng-data cg="215." f="560.734" m="657.917" t="0.369"/>\r
+<eng-data cg="215." f="587.738" m="616.412" t="0.511"/>\r
+<eng-data cg="215." f="603.86" m="572.136" t="0.657"/>\r
+<eng-data cg="215." f="612.022" m="537.169" t="0.77"/>\r
+<eng-data cg="215." f="625.75" m="434.474" t="1.096"/>\r
+<eng-data cg="215." f="620.083" m="351.403" t="1.358"/>\r
+<eng-data cg="215." f="612.022" m="267.052" t="1.627"/>\r
+<eng-data cg="215." f="603.86" m="201.45" t="1.839"/>\r
+<eng-data cg="215." f="590.459" m="135.188" t="2.057"/>\r
+<eng-data cg="215." f="598.52" m="86.4699" t="2.218"/>\r
+<eng-data cg="215." f="609.301" m="50.5051" t="2.335"/>\r
+<eng-data cg="215." f="601.24" m="35.1009" t="2.385"/>\r
+<eng-data cg="215." f="585.018" m="28.459" t="2.407"/>\r
+<eng-data cg="215." f="533.831" m="23.0488" t="2.426"/>\r
+<eng-data cg="215." f="385.511" m="13.4559" t="2.467"/>\r
+<eng-data cg="215." f="283.037" m="6.65001" t="2.507"/>\r
+<eng-data cg="215." f="164.441" m="2.66408" t="2.542"/>\r
+<eng-data cg="215." f="67.399" m="0.657965" t="2.576"/>\r
+<eng-data cg="215." f="29.653" m="0.188668" t="2.595"/>\r
+<eng-data cg="215." f="0." m="0." t="2.62"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works K570 White Wolf\r
-K570WW 54 492 0 0.9146 1.8151 AMW\r
-0.020 364.42\r
-0.030 664.79\r
-0.051 751.47\r
-0.071 745.81\r
-0.096 705.25\r
-0.137 674.93\r
-0.284 661.38\r
-0.528 651.24\r
-0.913 644.51\r
-1.192 651.24\r
-1.430 651.24\r
-1.649 651.24\r
-1.872 644.51\r
-2.176 624.23\r
-2.318 600.64\r
-2.394 597.33\r
-2.455 546.63\r
-2.501 485.89\r
-2.562 421.84\r
-2.597 340.83\r
-2.638 266.54\r
-2.734 175.48\r
-2.836 97.86\r
-2.927 47.24\r
-3.040 0.00\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="189.27" Itot="1697.59" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="558.419" burn-time="3.04" cgDiv="10" cgFix="1" cgStep="-1." code="K570WW" delays="1000" dia="54." exitDia="0." initWt="1815.1" len="492." mDiv="10" mFix="1" mStep="-1." massFrac="50.39" mfg="Animal Motor Works" peakThrust="751.47" propWt="914.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW K570 RASP.ENG file made from NAR published data\r
+File produced December 25, 2002\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="246." f="0." m="914.6" t="0."/>\r
+<eng-data cg="246." f="364.42" m="912.637" t="0.02"/>\r
+<eng-data cg="246." f="664.79" m="909.864" t="0.03"/>\r
+<eng-data cg="246." f="751.47" m="901.852" t="0.051"/>\r
+<eng-data cg="246." f="745.81" m="893.786" t="0.071"/>\r
+<eng-data cg="246." f="705.25" m="884.013" t="0.096"/>\r
+<eng-data cg="246." f="674.93" m="868.77" t="0.137"/>\r
+<eng-data cg="246." f="661.38" m="815.853" t="0.284"/>\r
+<eng-data cg="246." f="651.24" m="729.576" t="0.528"/>\r
+<eng-data cg="246." f="644.51" m="595.191" t="0.913"/>\r
+<eng-data cg="246." f="651.24" m="497.806" t="1.192"/>\r
+<eng-data cg="246." f="651.24" m="414.301" t="1.43"/>\r
+<eng-data cg="246." f="651.24" m="337.461" t="1.649"/>\r
+<eng-data cg="246." f="644.51" m="259.623" t="1.872"/>\r
+<eng-data cg="246." f="624.23" m="155.724" t="2.176"/>\r
+<eng-data cg="246." f="600.64" m="108.87" t="2.318"/>\r
+<eng-data cg="246." f="597.33" m="84.3437" t="2.394"/>\r
+<eng-data cg="246." f="546.63" m="65.5458" t="2.455"/>\r
+<eng-data cg="246." f="485.89" m="52.7513" t="2.501"/>\r
+<eng-data cg="246." f="421.84" m="37.8353" t="2.562"/>\r
+<eng-data cg="246." f="340.83" m="30.6445" t="2.597"/>\r
+<eng-data cg="246." f="266.54" m="23.9364" t="2.638"/>\r
+<eng-data cg="246." f="175.48" m="12.5055" t="2.734"/>\r
+<eng-data cg="246." f="97.86" m="4.99493" t="2.836"/>\r
+<eng-data cg="246." f="47.24" m="1.43799" t="2.927"/>\r
+<eng-data cg="246." f="0." m="0." t="3.04"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="208.34" Itot="2499.34" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="614.088" burn-time="4.07" cgDiv="10" cgFix="1" cgStep="-1." code="K600WW" delays="1000" dia="75." exitDia="0." initWt="2912.9" len="368." mDiv="10" mFix="1" mStep="-1." massFrac="42." mfg="Animal Motor Works" peakThrust="766.44" propWt="1223.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Animal Motor Works K600 RASP.ENG file made from NAR data\r
+File produced August 22, 2002\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="184." f="0." m="1223.3" t="0."/>\r
+<eng-data cg="184." f="412.229" m="1222.29" t="0.01"/>\r
+<eng-data cg="184." f="522.21" m="1217.95" t="0.029"/>\r
+<eng-data cg="184." f="547.215" m="1210.09" t="0.059"/>\r
+<eng-data cg="184." f="524.8" m="1203.8" t="0.083"/>\r
+<eng-data cg="184." f="497.305" m="1194.04" t="0.122"/>\r
+<eng-data cg="184." f="484.852" m="1179.86" t="0.181"/>\r
+<eng-data cg="184." f="495.113" m="1143.41" t="0.333"/>\r
+<eng-data cg="184." f="560.464" m="1051.19" t="0.69"/>\r
+<eng-data cg="184." f="643.548" m="902.388" t="1.195"/>\r
+<eng-data cg="184." f="673.833" m="836.297" t="1.4"/>\r
+<eng-data cg="184." f="708.799" m="829.53" t="1.42"/>\r
+<eng-data cg="184." f="701.427" m="799.159" t="1.508"/>\r
+<eng-data cg="184." f="721.551" m="770.256" t="1.591"/>\r
+<eng-data cg="184." f="731.712" m="702.327" t="1.782"/>\r
+<eng-data cg="184." f="752.035" m="616.996" t="2.017"/>\r
+<eng-data cg="184." f="756.816" m="559.023" t="2.174"/>\r
+<eng-data cg="184." f="765.2" m="528.108" t="2.257"/>\r
+<eng-data cg="184." f="766.44" m="436.274" t="2.502"/>\r
+<eng-data cg="184." f="752.931" m="352.613" t="2.727"/>\r
+<eng-data cg="184." f="738.187" m="282.915" t="2.918"/>\r
+<eng-data cg="184." f="705.91" m="203.398" t="3.143"/>\r
+<eng-data cg="184." f="643.847" m="115.864" t="3.408"/>\r
+<eng-data cg="184." f="569.131" m="57.979" t="3.603"/>\r
+<eng-data cg="184." f="526.793" m="34.1092" t="3.692"/>\r
+<eng-data cg="184." f="439.426" m="21.577" t="3.745"/>\r
+<eng-data cg="184." f="289.596" m="11.9429" t="3.799"/>\r
+<eng-data cg="184." f="112.272" m="3.68171" t="3.883"/>\r
+<eng-data cg="184." f="64.862" m="1.9911" t="3.922"/>\r
+<eng-data cg="184." f="37.437" m="0.764376" t="3.971"/>\r
+<eng-data cg="184." f="22.474" m="0.412496" t="3.995"/>\r
+<eng-data cg="184." f="0." m="0." t="4.07"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works K600 White Wolf\r
-K600WW 75 368 0 1.2233 2.9129 AMW\r
-0.010 412.229\r
-0.029 522.21\r
-0.059 547.215\r
-0.083 524.8\r
-0.122 497.305\r
-0.181 484.852\r
-0.333 495.113\r
-0.690 560.464\r
-1.195 643.548\r
-1.400 673.833\r
-1.420 708.799\r
-1.508 701.427\r
-1.591 721.551\r
-1.782 731.712\r
-2.017 752.035\r
-2.174 756.816\r
-2.257 765.2\r
-2.502 766.44\r
-2.727 752.931\r
-2.918 738.187\r
-3.143 705.91\r
-3.408 643.847\r
-3.603 569.131\r
-3.692 526.793\r
-3.745 439.426\r
-3.799 289.596\r
-3.883 112.272\r
-3.922 64.862\r
-3.971 37.437\r
-3.995 22.474\r
-4.070 0\r
+++ /dev/null
-;\r
-;AMW K605 RASP.ENG file made from NAR published data\r
-;File produced April 19, 2004\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-K605RR 75 368 100 1.231 2.7688 Animal_Motor_Works \r
-0.03 165.845\r
-0.053 309.12\r
-0.077 361.916\r
-0.142 392.042\r
-0.527 501.412\r
-0.988 606.905\r
-1.515 682.37\r
-2.101 730.593\r
-2.355 737.58\r
-2.692 731.289\r
-3 712.497\r
-3.361 671.036\r
-3.503 663.479\r
-3.586 659.701\r
-3.645 633.353\r
-3.692 573\r
-3.734 444.838\r
-3.775 297.785\r
-3.828 162.066\r
-3.864 98.015\r
-3.905 41.471\r
-3.95 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="198.9" Itot="2401.13" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="607.882" burn-time="3.95" cgDiv="10" cgFix="1" cgStep="-1." code="K605RR" delays="1000" dia="75." exitDia="0." initWt="2768.8" len="368." mDiv="10" mFix="1" mStep="-1." massFrac="44.46" mfg="Animal Motor Works" peakThrust="737.58" propWt="1231." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW K605 RASP.ENG file made from NAR published data\r
+File produced April 19, 2004\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="184." f="0." m="1231." t="0."/>\r
+<eng-data cg="184." f="165.845" m="1229.72" t="0.03"/>\r
+<eng-data cg="184." f="309.12" m="1226.92" t="0.053"/>\r
+<eng-data cg="184." f="361.916" m="1222.8" t="0.077"/>\r
+<eng-data cg="184." f="392.042" m="1210.23" t="0.142"/>\r
+<eng-data cg="184." f="501.412" m="1122.06" t="0.527"/>\r
+<eng-data cg="184." f="606.905" m="991.087" t="0.988"/>\r
+<eng-data cg="184." f="682.37" m="816.92" t="1.515"/>\r
+<eng-data cg="184." f="730.593" m="604.673" t="2.101"/>\r
+<eng-data cg="184." f="737.58" m="509.081" t="2.355"/>\r
+<eng-data cg="184." f="731.289" m="382.192" t="2.692"/>\r
+<eng-data cg="184." f="712.497" m="268.202" t="3."/>\r
+<eng-data cg="184." f="671.036" m="140.173" t="3.361"/>\r
+<eng-data cg="184." f="663.479" m="91.5969" t="3.503"/>\r
+<eng-data cg="184." f="659.701" m="63.4449" t="3.586"/>\r
+<eng-data cg="184." f="633.353" m="43.8889" t="3.645"/>\r
+<eng-data cg="184." f="573." m="29.3549" t="3.692"/>\r
+<eng-data cg="184." f="444.838" m="18.3967" t="3.734"/>\r
+<eng-data cg="184." f="297.785" m="10.5919" t="3.775"/>\r
+<eng-data cg="184." f="162.066" m="4.34441" t="3.828"/>\r
+<eng-data cg="184." f="98.015" m="1.94435" t="3.864"/>\r
+<eng-data cg="184." f="41.471" m="0.478375" t="3.905"/>\r
+<eng-data cg="184." f="0." m="0." t="3.95"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Animal Motor Works 54-1750\r
-; AMW K650RR RASP.ENG file made from NAR published data\r
-; File produced April 19, 2004\r
-; This file my be used or given away. All I ask is that this header \r
-; is maintained to give credit to NAR S&T. Thank you, Jack Kane\r
-; The total impulse, peak thrust, average thrust and burn time are\r
-; the same as the averaged static test data on the NAR web site in\r
-; the certification file. The curve drawn with these data points is as\r
-; close to the certification curve as can be with such a limited \r
-; number of points (32) allowed with wRASP up to v1.6.\r
-K650RR 54 492 0 0.931 1.8087 AMW\r
-0.022 308.257\r
-0.045 566.480\r
-0.058 620.440\r
-0.081 639.668\r
-0.135 639.668\r
-0.229 643.494\r
-0.351 662.823\r
-0.594 701.380\r
-0.810 724.434\r
-0.999 743.763\r
-1.151 751.220\r
-1.381 747.588\r
-1.610 736.001\r
-1.835 709.031\r
-2.073 685.876\r
-2.244 674.400\r
-2.334 682.051\r
-2.429 685.876\r
-2.469 666.648\r
-2.528 597.285\r
-2.573 481.714\r
-2.609 358.391\r
-2.631 250.471\r
-2.681 146.477\r
-2.721 65.507\r
-2.748 23.124\r
-2.770 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="199.5" Itot="1821.46" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="657.565" burn-time="2.77" cgDiv="10" cgFix="1" cgStep="-1." code="K650RR" delays="1000" dia="54." exitDia="0." initWt="1808.7" len="492." mDiv="10" mFix="1" mStep="-1." massFrac="51.47" mfg="Animal Motor Works" peakThrust="751.22" propWt="931." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW K650 RASP.ENG file made from NAR published data\r
+File produced April 19, 2004\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="246." f="0." m="931." t="0."/>\r
+<eng-data cg="246." f="308.257" m="929.267" t="0.022"/>\r
+<eng-data cg="246." f="566.48" m="924.125" t="0.045"/>\r
+<eng-data cg="246." f="620.44" m="920.182" t="0.058"/>\r
+<eng-data cg="246." f="639.668" m="912.775" t="0.081"/>\r
+<eng-data cg="246." f="639.668" m="895.119" t="0.135"/>\r
+<eng-data cg="246." f="643.494" m="864.294" t="0.229"/>\r
+<eng-data cg="246." f="662.823" m="823.564" t="0.351"/>\r
+<eng-data cg="246." f="701.38" m="738.844" t="0.594"/>\r
+<eng-data cg="246." f="724.434" m="660.137" t="0.81"/>\r
+<eng-data cg="246." f="743.763" m="589.22" t="0.999"/>\r
+<eng-data cg="246." f="751.22" m="531.146" t="1.151"/>\r
+<eng-data cg="246." f="747.588" m="443.047" t="1.381"/>\r
+<eng-data cg="246." f="736.001" m="356.22" t="1.61"/>\r
+<eng-data cg="246." f="709.031" m="273.128" t="1.835"/>\r
+<eng-data cg="246." f="685.876" m="188.284" t="2.073"/>\r
+<eng-data cg="246." f="674.4" m="128.838" t="2.244"/>\r
+<eng-data cg="246." f="682.051" m="97.6381" t="2.334"/>\r
+<eng-data cg="246." f="685.876" m="64.4266" t="2.429"/>\r
+<eng-data cg="246." f="666.648" m="50.6004" t="2.469"/>\r
+<eng-data cg="246." f="597.285" m="31.5424" t="2.528"/>\r
+<eng-data cg="246." f="481.714" m="19.1334" t="2.573"/>\r
+<eng-data cg="246." f="358.391" m="11.4042" t="2.609"/>\r
+<eng-data cg="246." f="250.471" m="7.98091" t="2.631"/>\r
+<eng-data cg="246." f="146.477" m="2.90861" t="2.681"/>\r
+<eng-data cg="246." f="65.507" m="0.741589" t="2.721"/>\r
+<eng-data cg="246." f="23.124" m="0.130013" t="2.748"/>\r
+<eng-data cg="246." f="0." m="0." t="2.77"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="176.09" Itot="1751.06" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="668.342" burn-time="2.62" cgDiv="10" cgFix="1" cgStep="-1." code="K670GG" delays="1000" dia="54." exitDia="0." initWt="1914.5" len="492." mDiv="10" mFix="1" mStep="-1." massFrac="52.96" mfg="Animal Motor Works" peakThrust="804.56" propWt="1014." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW K670 RASP.ENG file made from NAR published data\r
+File produced SEPT 4, 2002\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="246." f="0." m="1014." t="0."/>\r
+<eng-data cg="246." f="294.05" m="1012.64" t="0.016"/>\r
+<eng-data cg="246." f="398.577" m="1008.83" t="0.035"/>\r
+<eng-data cg="246." f="506.292" m="995.466" t="0.086"/>\r
+<eng-data cg="246." f="496.428" m="976.014" t="0.153"/>\r
+<eng-data cg="246." f="506.093" m="943.794" t="0.264"/>\r
+<eng-data cg="246." f="558.108" m="883.093" t="0.461"/>\r
+<eng-data cg="246." f="629.553" m="793.341" t="0.722"/>\r
+<eng-data cg="246." f="688.044" m="693.771" t="0.983"/>\r
+<eng-data cg="246." f="714.051" m="639.778" t="1.116"/>\r
+<eng-data cg="246." f="785.795" m="606.34" t="1.193"/>\r
+<eng-data cg="246." f="788.784" m="507.865" t="1.409"/>\r
+<eng-data cg="246." f="804.56" m="356.547" t="1.737"/>\r
+<eng-data cg="246." f="781.41" m="201.796" t="2.074"/>\r
+<eng-data cg="246." f="764.87" m="147.623" t="2.195"/>\r
+<eng-data cg="246." f="781.211" m="133.746" t="2.226"/>\r
+<eng-data cg="246." f="764.77" m="110.917" t="2.277"/>\r
+<eng-data cg="246." f="751.517" m="57.7952" t="2.398"/>\r
+<eng-data cg="246." f="744.941" m="39.5973" t="2.44"/>\r
+<eng-data cg="246." f="718.834" m="27.7303" t="2.468"/>\r
+<eng-data cg="246." f="666.521" m="21.3125" t="2.484"/>\r
+<eng-data cg="246." f="418.107" m="8.43676" t="2.525"/>\r
+<eng-data cg="246." f="218.818" m="3.64197" t="2.551"/>\r
+<eng-data cg="246." f="120.768" m="1.47886" t="2.573"/>\r
+<eng-data cg="246." f="52.143" m="0.377436" t="2.595"/>\r
+<eng-data cg="246." f="0." m="0." t="2.62"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works K670 Green Gorilla\r
-K670GG 54 492 0 1.0140 1.9145 AMW\r
-0.016 294.05\r
-0.035 398.577\r
-0.086 506.292\r
-0.153 496.428\r
-0.264 506.093\r
-0.461 558.108\r
-0.722 629.553\r
-0.983 688.044\r
-1.116 714.051\r
-1.193 785.795\r
-1.409 788.784\r
-1.737 804.56\r
-2.074 781.41\r
-2.195 764.87\r
-2.226 781.211\r
-2.277 764.77\r
-2.398 751.517\r
-2.440 744.941\r
-2.468 718.834\r
-2.484 666.521\r
-2.525 418.107\r
-2.551 218.818\r
-2.573 120.768\r
-2.595 52.143\r
-2.620 0\r
+++ /dev/null
-;\r
-;AMW K700 RASP.ENG file made from NAR published data\r
-;File produced April 19, 2004\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-K700BB 54 430 100 0.754 1.4831 Animal_Motor_Works \r
-0.014 359.559\r
-0.022 625.425\r
-0.03 737.756\r
-0.047 771.505\r
-0.082 786.516\r
-0.106 771.505\r
-0.144 775.233\r
-0.272 786.516\r
-0.477 812.71\r
-0.693 842.632\r
-0.97 847.06\r
-1.283 838.904\r
-1.516 816.438\r
-1.706 801.427\r
-1.779 793.972\r
-1.811 775.233\r
-1.841 726.573\r
-1.873 625.425\r
-1.909 509.367\r
-1.95 393.208\r
-1.982 337.093\r
-2.035 292.16\r
-2.073 228.489\r
-2.111 153.535\r
-2.155 86.137\r
-2.193 37.446\r
-2.24 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="217.41" Itot="1607.6" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="717.677" burn-time="2.24" cgDiv="10" cgFix="1" cgStep="-1." code="K700BB" delays="1000" dia="54." exitDia="0." initWt="1483.1" len="430." mDiv="10" mFix="1" mStep="-1." massFrac="50.84" mfg="Animal Motor Works" peakThrust="847.06" propWt="754." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW K700 RASP.ENG file made from NAR published data\r
+File produced April 19, 2004\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="215." f="0." m="754." t="0."/>\r
+<eng-data cg="215." f="359.559" m="752.82" t="0.014"/>\r
+<eng-data cg="215." f="625.425" m="750.972" t="0.022"/>\r
+<eng-data cg="215." f="737.756" m="748.414" t="0.03"/>\r
+<eng-data cg="215." f="771.505" m="742.397" t="0.047"/>\r
+<eng-data cg="215." f="786.516" m="729.609" t="0.082"/>\r
+<eng-data cg="215." f="771.505" m="720.84" t="0.106"/>\r
+<eng-data cg="215." f="775.233" m="707.056" t="0.144"/>\r
+<eng-data cg="215." f="786.516" m="660.177" t="0.272"/>\r
+<eng-data cg="215." f="812.71" m="583.294" t="0.477"/>\r
+<eng-data cg="215." f="842.632" m="499.444" t="0.693"/>\r
+<eng-data cg="215." f="847.06" m="389.682" t="0.97"/>\r
+<eng-data cg="215." f="838.904" m="265.928" t="1.283"/>\r
+<eng-data cg="215." f="816.438" m="175.479" t="1.516"/>\r
+<eng-data cg="215." f="801.427" m="103.391" t="1.706"/>\r
+<eng-data cg="215." f="793.972" m="76.0788" t="1.779"/>\r
+<eng-data cg="215." f="775.233" m="64.3029" t="1.811"/>\r
+<eng-data cg="215." f="726.573" m="53.7372" t="1.841"/>\r
+<eng-data cg="215." f="625.425" m="43.5913" t="1.873"/>\r
+<eng-data cg="215." f="509.367" m="34.0109" t="1.909"/>\r
+<eng-data cg="215." f="393.208" m="25.3327" t="1.95"/>\r
+<eng-data cg="215." f="337.093" m="19.8523" t="1.982"/>\r
+<eng-data cg="215." f="292.16" m="12.0312" t="2.035"/>\r
+<eng-data cg="215." f="228.489" m="7.39147" t="2.073"/>\r
+<eng-data cg="215." f="153.535" m="3.98709" t="2.111"/>\r
+<eng-data cg="215." f="86.137" m="1.51403" t="2.155"/>\r
+<eng-data cg="215." f="37.446" m="0.412731" t="2.193"/>\r
+<eng-data cg="215." f="0." m="0." t="2.24"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; This file my be used or given away. All I ask is that this header \r
-; is maintained to give credit to NAR S&T. Thank you, Jack Kane\r
-; The total impulse, peak thrust, average thrust and burn time are\r
-; the same as the averaged static test data on the NAR web site in\r
-; the certification file. The curve drawn with these data points is as\r
-; close to the certification curve as can be with such a limited \r
-; number of points (32) allowed with wRASP up to v1.6.\r
-K800BB 54 492 0 0.9140 1.7866 AMW\r
-0.017 516.316\r
-0.035 745.845\r
-0.046 817.592\r
-0.090 860.560\r
-0.191 889.338\r
-0.270 908.424\r
-0.438 918.017\r
-0.689 945.892\r
-0.996 955.090\r
-1.325 922.713\r
-1.557 894.035\r
-1.726 874.949\r
-1.849 884.542\r
-1.920 894.035\r
-1.954 894.035\r
-1.984 855.863\r
-2.011 741.048\r
-2.049 592.859\r
-2.079 492.433\r
-2.113 430.280\r
-2.154 377.719\r
-2.196 329.854\r
-2.237 243.818\r
-2.275 152.986\r
-2.309 71.716\r
-2.339 33.465\r
-2.380 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="215.61" Itot="1932.58" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="812.008" burn-time="2.38" cgDiv="10" cgFix="1" cgStep="-1." code="K800BB" delays="1000" dia="54." exitDia="0." initWt="1786.6" len="492." mDiv="10" mFix="1" mStep="-1." massFrac="51.16" mfg="Animal Motor Works" peakThrust="955.09" propWt="914." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW K800 RASP.ENG file made from NAR published data\r
+File produced April 19, 2004\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="246." f="0." m="914." t="0."/>\r
+<eng-data cg="246." f="516.316" m="911.924" t="0.017"/>\r
+<eng-data cg="246." f="745.845" m="906.552" t="0.035"/>\r
+<eng-data cg="246." f="817.592" m="902.485" t="0.046"/>\r
+<eng-data cg="246." f="860.56" m="885.024" t="0.09"/>\r
+<eng-data cg="246." f="889.338" m="843.231" t="0.191"/>\r
+<eng-data cg="246." f="908.424" m="809.646" t="0.27"/>\r
+<eng-data cg="246." f="918.017" m="737.087" t="0.438"/>\r
+<eng-data cg="246." f="945.892" m="626.456" t="0.689"/>\r
+<eng-data cg="246." f="955.09" m="488.45" t="0.996"/>\r
+<eng-data cg="246." f="922.713" m="342.359" t="1.325"/>\r
+<eng-data cg="246." f="894.035" m="242.69" t="1.557"/>\r
+<eng-data cg="246." f="874.949" m="171.994" t="1.726"/>\r
+<eng-data cg="246." f="884.542" m="120.818" t="1.849"/>\r
+<eng-data cg="246." f="894.035" m="90.9564" t="1.92"/>\r
+<eng-data cg="246." f="894.035" m="76.5803" t="1.954"/>\r
+<eng-data cg="246." f="855.863" m="64.1662" t="1.984"/>\r
+<eng-data cg="246." f="741.048" m="53.9704" t="2.011"/>\r
+<eng-data cg="246." f="592.859" m="41.984" t="2.049"/>\r
+<eng-data cg="246." f="492.433" m="34.2848" t="2.079"/>\r
+<eng-data cg="246." f="430.28" m="26.8661" t="2.113"/>\r
+<eng-data cg="246." f="377.719" m="19.0323" t="2.154"/>\r
+<eng-data cg="246." f="329.854" m="12.0048" t="2.196"/>\r
+<eng-data cg="246." f="243.818" m="6.44289" t="2.237"/>\r
+<eng-data cg="246." f="152.986" m="2.87724" t="2.275"/>\r
+<eng-data cg="246." f="71.716" m="1.07062" t="2.309"/>\r
+<eng-data cg="246." f="33.465" m="0.324454" t="2.339"/>\r
+<eng-data cg="246." f="0." m="0." t="2.38"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="213.59" Itot="1858.76" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="943.534" burn-time="1.97" cgDiv="10" cgFix="1" cgStep="-1." code="K950ST" delays="1000" dia="54." exitDia="0." initWt="1794.9" len="492." mDiv="10" mFix="1" mStep="-1." massFrac="49.44" mfg="Animal Motor Works" peakThrust="1204.52" propWt="887.4" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW K950 RASP.ENG file made from NAR published data\r
+File produced SEPT 4, 2002\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="246." f="0." m="887.4" t="0."/>\r
+<eng-data cg="246." f="771.836" m="885.373" t="0.011"/>\r
+<eng-data cg="246." f="1204.52" m="878.769" t="0.025"/>\r
+<eng-data cg="246." f="1083.24" m="871.123" t="0.039"/>\r
+<eng-data cg="246." f="1158.05" m="863.633" t="0.053"/>\r
+<eng-data cg="246." f="1036.36" m="856.299" t="0.067"/>\r
+<eng-data cg="246." f="1110.18" m="847.076" t="0.085"/>\r
+<eng-data cg="246." f="1022.4" m="839.949" t="0.099"/>\r
+<eng-data cg="246." f="982.102" m="822.724" t="0.135"/>\r
+<eng-data cg="246." f="968.835" m="783.139" t="0.22"/>\r
+<eng-data cg="246." f="1010.43" m="696.206" t="0.404"/>\r
+<eng-data cg="246." f="1044.34" m="616.746" t="0.566"/>\r
+<eng-data cg="246." f="1079.25" m="548.313" t="0.701"/>\r
+<eng-data cg="246." f="1106.19" m="461.714" t="0.867"/>\r
+<eng-data cg="246." f="1134.12" m="393.262" t="0.995"/>\r
+<eng-data cg="246." f="1114.17" m="277.339" t="1.211"/>\r
+<eng-data cg="246." f="1101.2" m="223.398" t="1.313"/>\r
+<eng-data cg="246." f="1067.29" m="162.835" t="1.43"/>\r
+<eng-data cg="246." f="1020.4" m="113.499" t="1.529"/>\r
+<eng-data cg="246." f="993.772" m="89.459" t="1.579"/>\r
+<eng-data cg="246." f="892.43" m="61.0933" t="1.642"/>\r
+<eng-data cg="246." f="818.119" m="48.027" t="1.674"/>\r
+<eng-data cg="246." f="757.273" m="31.8566" t="1.717"/>\r
+<eng-data cg="246." f="621.918" m="24.9429" t="1.738"/>\r
+<eng-data cg="246." f="466.313" m="17.6694" t="1.766"/>\r
+<eng-data cg="246." f="351.306" m="12.7901" t="1.791"/>\r
+<eng-data cg="246." f="249.864" m="8.19795" t="1.823"/>\r
+<eng-data cg="246." f="175.553" m="3.93285" t="1.865"/>\r
+<eng-data cg="246." f="87.696" m="1.23075" t="1.908"/>\r
+<eng-data cg="246." f="33.654" m="0.216903" t="1.943"/>\r
+<eng-data cg="246." f="0." m="0." t="1.97"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works K950 Super Tiger\r
-K950ST 54 492 0 .8874 1.7949 AMW\r
-0.011 771.836\r
-0.025 1204.520\r
-0.039 1083.244\r
-0.053 1158.054\r
-0.067 1036.364\r
-0.085 1110.176\r
-0.099 1022.399\r
-0.135 982.102\r
-0.220 968.835\r
-0.404 1010.430\r
-0.566 1044.343\r
-0.701 1079.254\r
-0.867 1106.186\r
-0.995 1134.115\r
-1.211 1114.166\r
-1.313 1101.199\r
-1.430 1067.285\r
-1.529 1020.404\r
-1.579 993.772\r
-1.642 892.430\r
-1.674 818.119\r
-1.717 757.273\r
-1.738 621.918\r
-1.766 466.313\r
-1.791 351.306\r
-1.823 249.864\r
-1.865 175.553\r
-1.908 87.696\r
-1.943 33.654\r
-1.970 0.000\r
+++ /dev/null
-;\r
-;Animal Motor Works K975 White Wolf\r
-K975WW 54 728 0 1.357 2.5985 AMW\r
-0.017 526.644\r
-0.029 901.850\r
-0.038 1098.918\r
-0.046 1151.722\r
-0.076 1112.867\r
-0.130 1060.063\r
-0.219 1053.089\r
-0.336 1053.089\r
-0.479 1059.066\r
-0.609 1091.944\r
-0.866 1136.778\r
-1.046 1176.630\r
-1.164 1175.634\r
-1.202 1228.437\r
-1.239 1208.511\r
-1.315 1215.486\r
-1.353 1267.293\r
-1.387 1228.437\r
-1.487 1241.389\r
-1.538 1260.319\r
-1.634 1290.900\r
-1.723 1281.241\r
-1.794 1266.297\r
-1.836 1207.515\r
-1.933 1049.103\r
-1.992 851.437\r
-2.080 666.923\r
-2.118 640.521\r
-2.193 462.582\r
-2.269 212.311\r
-2.378 119.854\r
-2.510 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="184.4" Itot="2454.41" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="977.851" burn-time="2.51" cgDiv="10" cgFix="1" cgStep="-1." code="K975WW" delays="1000" dia="54." exitDia="0." initWt="2598.5" len="728." mDiv="10" mFix="1" mStep="-1." massFrac="52.23" mfg="Animal Motor Works" peakThrust="1290.9" propWt="1357.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW K975 RASP.ENG file made from NAR published data\r
+File produced December 25, 2002\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="364." f="0." m="1357.3" t="0."/>\r
+<eng-data cg="364." f="526.644" m="1354.82" t="0.017"/>\r
+<eng-data cg="364." f="901.85" m="1350.08" t="0.029"/>\r
+<eng-data cg="364." f="1098.92" m="1345.11" t="0.038"/>\r
+<eng-data cg="364." f="1151.72" m="1340.13" t="0.046"/>\r
+<eng-data cg="364." f="1112.87" m="1321.34" t="0.076"/>\r
+<eng-data cg="364." f="1060.06" m="1288.9" t="0.13"/>\r
+<eng-data cg="364." f="1053.09" m="1236.9" t="0.219"/>\r
+<eng-data cg="364." f="1053.09" m="1168.76" t="0.336"/>\r
+<eng-data cg="364." f="1059.07" m="1085.24" t="0.479"/>\r
+<eng-data cg="364." f="1091.94" m="1007.93" t="0.609"/>\r
+<eng-data cg="364." f="1136.78" m="849.55" t="0.866"/>\r
+<eng-data cg="364." f="1176.63" m="734.411" t="1.046"/>\r
+<eng-data cg="364." f="1175.63" m="657.663" t="1.164"/>\r
+<eng-data cg="364." f="1228.44" m="632.403" t="1.202"/>\r
+<eng-data cg="364." f="1208.51" m="607.472" t="1.239"/>\r
+<eng-data cg="364." f="1215.49" m="556.533" t="1.315"/>\r
+<eng-data cg="364." f="1267.29" m="530.446" t="1.353"/>\r
+<eng-data cg="364." f="1228.44" m="506.984" t="1.387"/>\r
+<eng-data cg="364." f="1241.39" m="438.692" t="1.487"/>\r
+<eng-data cg="364." f="1260.32" m="403.414" t="1.538"/>\r
+<eng-data cg="364." f="1290.9" m="335.694" t="1.634"/>\r
+<eng-data cg="364." f="1281.24" m="272.397" t="1.723"/>\r
+<eng-data cg="364." f="1266.3" m="222.384" t="1.794"/>\r
+<eng-data cg="364." f="1207.52" m="193.655" t="1.836"/>\r
+<eng-data cg="364." f="1049.1" m="133.131" t="1.933"/>\r
+<eng-data cg="364." f="851.437" m="102.126" t="1.992"/>\r
+<eng-data cg="364." f="666.923" m="65.1812" t="2.08"/>\r
+<eng-data cg="364." f="640.521" m="51.4437" t="2.118"/>\r
+<eng-data cg="364." f="462.582" m="28.5679" t="2.193"/>\r
+<eng-data cg="364." f="212.311" m="14.3855" t="2.269"/>\r
+<eng-data cg="364." f="119.854" m="4.37448" t="2.378"/>\r
+<eng-data cg="364." f="0." m="0." t="2.51"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="192.52" Itot="3622.74" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1065.51" burn-time="3.4" cgDiv="10" cgFix="1" cgStep="-1." code="L1060GG" delays="1000" dia="75." exitDia="0." initWt="3938.8" len="497." mDiv="10" mFix="1" mStep="-1." massFrac="48.72" mfg="Animal Motor Works" peakThrust="1298.25" propWt="1918.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW L1060 RASP.ENG file made from NAR published data\r
+File produced August 22, 2002\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="248.5" f="0." m="1918.8" t="0."/>\r
+<eng-data cg="248.5" f="258.773" m="1917.43" t="0.02"/>\r
+<eng-data cg="248.5" f="368.235" m="1916.77" t="0.024"/>\r
+<eng-data cg="248.5" f="328.386" m="1915.29" t="0.032"/>\r
+<eng-data cg="248.5" f="427.96" m="1906.48" t="0.076"/>\r
+<eng-data cg="248.5" f="567.284" m="1900.15" t="0.1"/>\r
+<eng-data cg="248.5" f="751.352" m="1894.56" t="0.116"/>\r
+<eng-data cg="248.5" f="791.202" m="1889.66" t="0.128"/>\r
+<eng-data cg="248.5" f="816.071" m="1872.21" t="0.169"/>\r
+<eng-data cg="248.5" f="816.071" m="1848." t="0.225"/>\r
+<eng-data cg="248.5" f="875.795" m="1810.37" t="0.309"/>\r
+<eng-data cg="248.5" f="985.257" m="1707.36" t="0.518"/>\r
+<eng-data cg="248.5" f="1079.64" m="1573.38" t="0.763"/>\r
+<eng-data cg="248.5" f="1174.52" m="1417.58" t="1.024"/>\r
+<eng-data cg="248.5" f="1229.45" m="1236.77" t="1.308"/>\r
+<eng-data cg="248.5" f="1288.38" m="1038.07" t="1.606"/>\r
+<eng-data cg="248.5" f="1298.25" m="917.506" t="1.782"/>\r
+<eng-data cg="248.5" f="1293.37" m="779.553" t="1.983"/>\r
+<eng-data cg="248.5" f="1239.44" m="596.436" t="2.256"/>\r
+<eng-data cg="248.5" f="1184.51" m="423.757" t="2.525"/>\r
+<eng-data cg="248.5" f="1129.58" m="241.746" t="2.822"/>\r
+<eng-data cg="248.5" f="1069.65" m="115.944" t="3.038"/>\r
+<eng-data cg="248.5" f="1044.68" m="75.0684" t="3.111"/>\r
+<eng-data cg="248.5" f="995.145" m="62.1036" t="3.135"/>\r
+<eng-data cg="248.5" f="835.946" m="38.8273" t="3.183"/>\r
+<eng-data cg="248.5" f="552.303" m="18.239" t="3.239"/>\r
+<eng-data cg="248.5" f="268.661" m="5.19421" t="3.299"/>\r
+<eng-data cg="248.5" f="164.193" m="1.98452" t="3.327"/>\r
+<eng-data cg="248.5" f="84.593" m="1.1939" t="3.339"/>\r
+<eng-data cg="248.5" f="44.783" m="0.474391" t="3.36"/>\r
+<eng-data cg="248.5" f="0." m="0." t="3.4"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works L1060 Green Gorilla\r
-L1060GG 75 497 0 1.9188 3.9388 AMW\r
-0.020 258.773\r
-0.024 368.235\r
-0.032 328.386\r
-0.076 427.96\r
-0.100 567.284\r
-0.116 751.352\r
-0.128 791.202\r
-0.169 816.071\r
-0.225 816.071\r
-0.309 875.795\r
-0.518 985.257\r
-0.763 1079.639\r
-1.024 1174.519\r
-1.308 1229.45\r
-1.606 1288.375\r
-1.782 1298.25\r
-1.983 1293.369\r
-2.256 1239.437\r
-2.525 1184.506\r
-2.822 1129.576\r
-3.038 1069.651\r
-3.111 1044.683\r
-3.135 995.145\r
-3.183 835.946\r
-3.239 552.303\r
-3.299 268.661\r
-3.327 164.193\r
-3.339 84.593\r
-3.360 44.783\r
-3.400 0\r
+++ /dev/null
-;\r
-;AMW L1080 RASP.ENG file made from NAR published data\r
-;File produced April 19, 2004\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-L1080BB 75 497 100 1.717 3.5922 Animal_Motor_Works \r
-0.024 406.295\r
-0.043 812.489\r
-0.052 895.202\r
-0.088 929.641\r
-0.314 991.55\r
-0.626 1087.69\r
-0.988 1163.44\r
-1.346 1218.99\r
-1.638 1246.25\r
-1.864 1257.91\r
-2.247 1254.84\r
-2.6 1218.99\r
-2.766 1211.92\r
-2.851 1197.78\r
-2.942 1204.85\r
-3.002 1226.06\r
-3.033 1204.85\r
-3.089 1040.23\r
-3.124 874.499\r
-3.15 660.999\r
-3.191 461.336\r
-3.232 275.408\r
-3.268 144.622\r
-3.303 75.744\r
-3.339 41.316\r
-3.39 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="218.92" Itot="3686.19" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1087.37" burn-time="3.39" cgDiv="10" cgFix="1" cgStep="-1." code="L1080BB" delays="1000" dia="75." exitDia="0." initWt="3592.2" len="497." mDiv="10" mFix="1" mStep="-1." massFrac="47.8" mfg="Animal Motor Works" peakThrust="1257.91" propWt="1717." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW L1080 RASP.ENG file made from NAR published data\r
+File produced April 19, 2004\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="248.5" f="0." m="1717." t="0."/>\r
+<eng-data cg="248.5" f="406.295" m="1714.73" t="0.024"/>\r
+<eng-data cg="248.5" f="812.489" m="1709.34" t="0.043"/>\r
+<eng-data cg="248.5" f="895.202" m="1705.76" t="0.052"/>\r
+<eng-data cg="248.5" f="929.641" m="1690.46" t="0.088"/>\r
+<eng-data cg="248.5" f="991.55" m="1589.34" t="0.314"/>\r
+<eng-data cg="248.5" f="1087.69" m="1438.25" t="0.626"/>\r
+<eng-data cg="248.5" f="1163.44" m="1248.46" t="0.988"/>\r
+<eng-data cg="248.5" f="1218.99" m="1049.82" t="1.346"/>\r
+<eng-data cg="248.5" f="1246.25" m="882.172" t="1.638"/>\r
+<eng-data cg="248.5" f="1257.91" m="750.366" t="1.864"/>\r
+<eng-data cg="248.5" f="1254.84" m="526.231" t="2.247"/>\r
+<eng-data cg="248.5" f="1218.99" m="322.852" t="2.6"/>\r
+<eng-data cg="248.5" f="1211.92" m="228.871" t="2.766"/>\r
+<eng-data cg="248.5" f="1197.78" m="181.168" t="2.851"/>\r
+<eng-data cg="248.5" f="1204.85" m="130.248" t="2.942"/>\r
+<eng-data cg="248.5" f="1226.06" m="96.2789" t="3.002"/>\r
+<eng-data cg="248.5" f="1204.85" m="78.7283" t="3.033"/>\r
+<eng-data cg="248.5" f="1040.23" m="49.4475" t="3.089"/>\r
+<eng-data cg="248.5" f="874.499" m="33.8399" t="3.124"/>\r
+<eng-data cg="248.5" f="660.999" m="24.542" t="3.15"/>\r
+<eng-data cg="248.5" f="461.336" m="13.8251" t="3.191"/>\r
+<eng-data cg="248.5" f="275.408" m="6.79012" t="3.232"/>\r
+<eng-data cg="248.5" f="144.622" m="3.26848" t="3.268"/>\r
+<eng-data cg="248.5" f="75.744" m="1.4722" t="3.303"/>\r
+<eng-data cg="248.5" f="41.316" m="0.490739" t="3.339"/>\r
+<eng-data cg="248.5" f="0." m="0." t="3.39"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="195.17" Itot="2576.19" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1096.25" burn-time="2.35" cgDiv="10" cgFix="1" cgStep="-1." code="L1100SM" delays="1000" dia="54." exitDia="0." initWt="2588.1" len="728." mDiv="10" mFix="1" mStep="-1." massFrac="52.01" mfg="Animal Motor Works" peakThrust="1340.23" propWt="1346." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW L1100 RASP.ENG file made from NAR published data\r
+File produced April 19, 2004\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="364." f="0." m="1346." t="0."/>\r
+<eng-data cg="364." f="681.489" m="1343.69" t="0.013"/>\r
+<eng-data cg="364." f="1116.88" m="1336.17" t="0.029"/>\r
+<eng-data cg="364." f="1196.3" m="1328.92" t="0.041"/>\r
+<eng-data cg="364." f="1210.38" m="1305.03" t="0.079"/>\r
+<eng-data cg="364." f="1203.34" m="1262.15" t="0.147"/>\r
+<eng-data cg="364." f="1218.42" m="1192.56" t="0.257"/>\r
+<eng-data cg="364." f="1225.45" m="1122.97" t="0.366"/>\r
+<eng-data cg="364." f="1254.61" m="992.742" t="0.567"/>\r
+<eng-data cg="364." f="1282.76" m="822.387" t="0.824"/>\r
+<eng-data cg="364." f="1311.91" m="663.098" t="1.059"/>\r
+<eng-data cg="364." f="1340.23" m="518.987" t="1.267"/>\r
+<eng-data cg="364." f="1311.91" m="385.962" t="1.459"/>\r
+<eng-data cg="364." f="1297.84" m="274.834" t="1.622"/>\r
+<eng-data cg="364." f="1290.8" m="213.295" t="1.713"/>\r
+<eng-data cg="364." f="1268.68" m="165.153" t="1.785"/>\r
+<eng-data cg="364." f="1218.42" m="135.915" t="1.83"/>\r
+<eng-data cg="364." f="1080.69" m="102.281" t="1.886"/>\r
+<eng-data cg="364." f="819.214" m="61.0857" t="1.969"/>\r
+<eng-data cg="364." f="558.24" m="32.6581" t="2.048"/>\r
+<eng-data cg="364." f="376.985" m="17.9991" t="2.108"/>\r
+<eng-data cg="364." f="246.498" m="10.1809" t="2.156"/>\r
+<eng-data cg="364." f="144.963" m="5.16998" t="2.205"/>\r
+<eng-data cg="364." f="72.501" m="1.53414" t="2.269"/>\r
+<eng-data cg="364." f="0." m="0." t="2.35"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;L1111ST entered by Tim Van Milligan\r
-;For RockSim - http://www.rocksim.com\r
-;Based on TRA Certification paperwork from 06-01-2002\r
-;Initial Mass from Jim Robinson at AMW\r
-;Not approved by TRA or AMW.\r
-L1111ST 75 497 100 1.642 3.517 Animal_Motor_Works \r
-0.015 1023.97\r
-0.1 924.878\r
-0.147 902.857\r
-0.502 1034.98\r
-0.75 1156.1\r
-1.005 1266.2\r
-1.229 1354.29\r
-1.492 1398.33\r
-1.739 1398.33\r
-2.009 1354.29\r
-2.272 1244.18\r
-2.504 1123.07\r
-2.728 968.92\r
-2.782 902.857\r
-2.836 770.732\r
-2.98 363.345\r
-3.053 99.094\r
-3.083 22.021\r
-3.14 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="215.97" Itot="3477.72" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1107.55" burn-time="3.14" cgDiv="10" cgFix="1" cgStep="-1." code="L1111ST" delays="1000" dia="76." exitDia="0." initWt="3517." len="497." mDiv="10" mFix="1" mStep="-1." massFrac="46.69" mfg="Animal Motor Works" peakThrust="1398.33" propWt="1642." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>L1111ST entered by Tim Van Milligan\r
+For RockSim - http://www.rocksim.com\r
+Based on TRA Certification paperwork from 06-01-2002\r
+Initial Mass from Jim Robinson at AMW\r
+Not approved by TRA or AMW.\r
+</comments>\r
+<data>\r
+<eng-data cg="248.5" f="0." m="1642." t="0."/>\r
+<eng-data cg="248.5" f="1023.97" m="1638.37" t="0.015"/>\r
+<eng-data cg="248.5" f="924.878" m="1599.27" t="0.1"/>\r
+<eng-data cg="248.5" f="902.857" m="1578.99" t="0.147"/>\r
+<eng-data cg="248.5" f="1034.98" m="1416.59" t="0.502"/>\r
+<eng-data cg="248.5" f="1156.1" m="1288.31" t="0.75"/>\r
+<eng-data cg="248.5" f="1266.2" m="1142.49" t="1.005"/>\r
+<eng-data cg="248.5" f="1354.29" m="1003.91" t="1.229"/>\r
+<eng-data cg="248.5" f="1398.33" m="833.009" t="1.492"/>\r
+<eng-data cg="248.5" f="1398.33" m="669.935" t="1.739"/>\r
+<eng-data cg="248.5" f="1354.29" m="494.483" t="2.009"/>\r
+<eng-data cg="248.5" f="1244.18" m="333.151" t="2.272"/>\r
+<eng-data cg="248.5" f="1123.07" m="203.498" t="2.504"/>\r
+<eng-data cg="248.5" f="968.92" m="92.8724" t="2.728"/>\r
+<eng-data cg="248.5" f="902.857" m="69.011" t="2.782"/>\r
+<eng-data cg="248.5" f="770.732" m="47.6761" t="2.836"/>\r
+<eng-data cg="248.5" f="363.345" m="9.12349" t="2.98"/>\r
+<eng-data cg="248.5" f="99.094" m="1.15408" t="3.053"/>\r
+<eng-data cg="248.5" f="22.021" m="0.29632" t="3.083"/>\r
+<eng-data cg="248.5" f="0." m="0." t="3.14"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;AMW L1300 RASP.ENG file made from NAR published data\r
-;File produced April 19, 2004\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-L1300BB 75 728 100 1.314 2.5454 Animal_Motor_Works \r
-0.014 710.467\r
-0.025 1247.64\r
-0.039 1384.13\r
-0.053 1447.83\r
-0.074 1420.53\r
-0.12 1447.83\r
-0.276 1474.12\r
-0.475 1519.61\r
-0.712 1555\r
-0.942 1586.74\r
-1.147 1562.08\r
-1.36 1534.78\r
-1.484 1551.97\r
-1.537 1551.97\r
-1.569 1497.37\r
-1.59 1406.38\r
-1.604 1451.87\r
-1.615 1333.58\r
-1.64 1168.78\r
-1.689 986.687\r
-1.753 767.749\r
-1.824 512.503\r
-1.891 275.512\r
-1.933 147.816\r
-1.987 74.737\r
-2.06 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="207.36" Itot="2672.02" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1297.1" burn-time="2.06" cgDiv="10" cgFix="1" cgStep="-1." code="L1300BB" delays="1000" dia="54." exitDia="0." initWt="2545.4" len="728." mDiv="10" mFix="1" mStep="-1." massFrac="51.62" mfg="Animal Motor Works" peakThrust="1586.74" propWt="1314." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW L1300 RASP.ENG file made from NAR published data\r
+File produced April 19, 2004\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="364." f="0." m="1314." t="0."/>\r
+<eng-data cg="364." f="710.467" m="1311.55" t="0.014"/>\r
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+<eng-data cg="364." f="1497.37" m="145.326" t="1.569"/>\r
+<eng-data cg="364." f="1406.38" m="130.333" t="1.59"/>\r
+<eng-data cg="364." f="1451.87" m="120.494" t="1.604"/>\r
+<eng-data cg="364." f="1333.58" m="112.96" t="1.615"/>\r
+<eng-data cg="364." f="1168.78" m="97.578" t="1.64"/>\r
+<eng-data cg="364." f="986.687" m="71.6085" t="1.689"/>\r
+<eng-data cg="364." f="767.749" m="44." t="1.753"/>\r
+<eng-data cg="364." f="512.503" m="21.6499" t="1.824"/>\r
+<eng-data cg="364." f="275.512" m="8.66816" t="1.891"/>\r
+<eng-data cg="364." f="147.816" m="4.29644" t="1.933"/>\r
+<eng-data cg="364." f="74.737" m="1.34148" t="1.987"/>\r
+<eng-data cg="364." f="0." m="0." t="2.06"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; @File: SK-75-6000.txt, @Pts-I: 3609, @Pts-O: 31, @Sm: 6, @CO: 5%\r
-; @TI: 4740.56, @TIa: 4732.91, @TIe: 0.0%, @ThMax: 1908.398, @ThAvg: 1382.678, @Tb: 3.423\r
-; Exported using ThrustCurveTool, www.ThrustGear.com, by John DeMar\r
-L1400SK 75 785 P 2.8267 5.1985 AMW\r
- 0.0 68.1234\r
- 0.0040 193.7893\r
- 0.016 690.259\r
- 0.021 814.579\r
- 0.027 900.741\r
- 0.045 997.475\r
- 0.076 1251.156\r
- 0.092 1354.553\r
- 0.107 1405.971\r
- 0.132 1440.082\r
- 0.169 1453.774\r
- 0.368 1397.446\r
- 0.525 1411.875\r
- 0.705 1488.288\r
- 1.082 1734.489\r
- 1.414 1906.629\r
- 1.556 1875.238\r
- 1.766 1882.261\r
- 1.899 1803.008\r
- 2.142 1745.497\r
- 2.34 1659.082\r
- 2.504 1522.458\r
- 2.58 1402.287\r
- 2.819 844.839\r
- 2.847 841.674\r
- 2.893 730.795\r
- 3.068 406.536\r
- 3.176 265.8\r
- 3.425 94.9644\r
- 3.608 0.874524\r
- 3.609 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Animal Motor Works" code="L1400SK" Type="reloadable" dia="75." len="785."\r
+initWt="5198.5" propWt="2826.7" delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="1313.57" peakThrust="1906.63" throatDia="0." exitDia="0."\r
+Itot="4740.66" burn-time="3.61" massFrac="54.38" Isp="171.02" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>@File: SK-75-6000.txt, @Pts-I: 3609, @Pts-O: 31, @Sm: 6, @CO: 5%\r
+@TI: 4740.56, @TIa: 4732.91, @TIe: 0.0%, @ThMax: 1908.398, @ThAvg: 1382.678, @Tb: 3.423\r
+Exported using ThrustCurveTool, www.ThrustGear.com, by John DeMar\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="2826.7" cg="392.5"/>\r
+<eng-data t="0." f="68.1234" m="2826.7" cg="392.5"/>\r
+<eng-data t="0.004" f="193.789" m="2826.39" cg="392.5"/>\r
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+<eng-data t="0.021" f="814.579" m="2820.98" cg="392.5"/>\r
+<eng-data t="0.027" f="900.741" m="2817.91" cg="392.5"/>\r
+<eng-data t="0.045" f="997.475" m="2807.73" cg="392.5"/>\r
+<eng-data t="0.076" f="1251.16" m="2786.94" cg="392.5"/>\r
+<eng-data t="0.092" f="1354.55" m="2774.51" cg="392.5"/>\r
+<eng-data t="0.107" f="1405.97" m="2762.17" cg="392.5"/>\r
+<eng-data t="0.132" f="1440.08" m="2740.96" cg="392.5"/>\r
+<eng-data t="0.169" f="1453.77" m="2709.04" cg="392.5"/>\r
+<eng-data t="0.368" f="1397.45" m="2539.88" cg="392.5"/>\r
+<eng-data t="0.525" f="1411.88" m="2408.38" cg="392.5"/>\r
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+<eng-data t="1.082" f="1734.49" m="1890.52" cg="392.5"/>\r
+<eng-data t="1.414" f="1906.63" m="1530.12" cg="392.5"/>\r
+<eng-data t="1.556" f="1875.24" m="1370.01" cg="392.5"/>\r
+<eng-data t="1.766" f="1882.26" m="1134.76" cg="392.5"/>\r
+<eng-data t="1.899" f="1803.01" m="988.635" cg="392.5"/>\r
+<eng-data t="2.142" f="1745.5" m="731.559" cg="392.5"/>\r
+<eng-data t="2.34" f="1659.08" m="530.585" cg="392.5"/>\r
+<eng-data t="2.504" f="1522.46" m="375.027" cg="392.5"/>\r
+<eng-data t="2.58" f="1402.29" m="308.757" cg="392.5"/>\r
+<eng-data t="2.819" f="844.839" m="148.641" cg="392.5"/>\r
+<eng-data t="2.847" f="841.674" m="134.562" cg="392.5"/>\r
+<eng-data t="2.893" f="730.795" m="112.997" cg="392.5"/>\r
+<eng-data t="3.068" f="406.536" m="53.6587" cg="392.5"/>\r
+<eng-data t="3.176" f="265.8" m="32.0105" cg="392.5"/>\r
+<eng-data t="3.425" f="94.9644" m="5.22909" cg="392.5"/>\r
+<eng-data t="3.608" f="0.874524" m="0.000260725" cg="392.5"/>\r
+<eng-data t="3.609" f="0." m="0." cg="392.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;Animal Motor Works 75-3500\r
-L666SK 75 497 0 1.8877 3.5344 AMW\r
-0.096 105.880\r
-0.175 509.783\r
-0.312 549.481\r
-0.449 577.319\r
-0.586 602.900\r
-0.722 615.605\r
-0.859 632.540\r
-0.996 652.072\r
-1.133 671.418\r
-1.270 685.671\r
-1.407 701.286\r
-1.543 718.069\r
-1.680 734.116\r
-1.817 753.292\r
-1.954 771.589\r
-2.091 790.453\r
-2.228 819.222\r
-2.364 846.663\r
-2.501 874.629\r
-2.638 890.083\r
-2.775 898.271\r
-2.912 899.312\r
-3.049 881.683\r
-3.185 845.157\r
-3.322 768.451\r
-3.459 672.771\r
-3.596 525.466\r
-3.733 304.694\r
-3.870 86.663\r
-3.968 0.000\r
-;\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Animal Motor Works" code="L666SK" Type="reloadable" dia="75." len="497."\r
+initWt="3534.4" propWt="1887.7" delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="663.042" peakThrust="899.312" throatDia="0." exitDia="0."\r
+Itot="2630.95" burn-time="3.97" massFrac="53.41" Isp="142.12" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Animal Motor Works 75-3500</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="1887.7" cg="248.5"/>\r
+<eng-data t="0.096" f="105.88" m="1884.05" cg="248.5"/>\r
+<eng-data t="0.175" f="509.783" m="1866.6" cg="248.5"/>\r
+<eng-data t="0.312" f="549.481" m="1814.54" cg="248.5"/>\r
+<eng-data t="0.449" f="577.319" m="1759.16" cg="248.5"/>\r
+<eng-data t="0.586" f="602.9" m="1701.16" cg="248.5"/>\r
+<eng-data t="0.722" f="615.605" m="1641.71" cg="248.5"/>\r
+<eng-data t="0.859" f="632.54" m="1580.36" cg="248.5"/>\r
+<eng-data t="0.996" f="652.072" m="1517.23" cg="248.5"/>\r
+<eng-data t="1.133" f="671.418" m="1452.18" cg="248.5"/>\r
+<eng-data t="1.27" f="685.671" m="1385.48" cg="248.5"/>\r
+<eng-data t="1.407" f="701.286" m="1317.31" cg="248.5"/>\r
+<eng-data t="1.543" f="718.069" m="1248.06" cg="248.5"/>\r
+<eng-data t="1.68" f="734.116" m="1176.69" cg="248.5"/>\r
+<eng-data t="1.817" f="753.292" m="1103.58" cg="248.5"/>\r
+<eng-data t="1.954" f="771.589" m="1028.64" cg="248.5"/>\r
+<eng-data t="2.091" f="790.453" m="951.867" cg="248.5"/>\r
+<eng-data t="2.228" f="819.222" m="872.754" cg="248.5"/>\r
+<eng-data t="2.364" f="846.663" m="791.476" cg="248.5"/>\r
+<eng-data t="2.501" f="874.629" m="706.877" cg="248.5"/>\r
+<eng-data t="2.638" f="890.083" m="620.144" cg="248.5"/>\r
+<eng-data t="2.775" f="898.271" m="532.249" cg="248.5"/>\r
+<eng-data t="2.912" f="899.312" m="443.9" cg="248.5"/>\r
+<eng-data t="3.049" f="881.683" m="356.367" cg="248.5"/>\r
+<eng-data t="3.185" f="845.157" m="272.115" cg="248.5"/>\r
+<eng-data t="3.322" f="768.451" m="192.808" cg="248.5"/>\r
+<eng-data t="3.459" f="672.771" m="121.974" cg="248.5"/>\r
+<eng-data t="3.596" f="525.466" m="63.0826" cg="248.5"/>\r
+<eng-data t="3.733" f="304.694" m="22.2815" cg="248.5"/>\r
+<eng-data t="3.87" f="86.663" m="3.04684" cg="248.5"/>\r
+<eng-data t="3.968" f="0." m="0." cg="248.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-L700BB 75.0 368.00 100 1.19310 2.73200 AMW\r
- 0.02 221.87 \r
- 0.03 399.33 \r
- 0.05 467.56 \r
- 0.08 494.89 \r
- 0.13 498.41 \r
- 0.24 535.99 \r
- 0.48 614.67 \r
- 0.77 683.20 \r
- 1.23 755.25 \r
- 1.62 789.72 \r
- 1.92 810.42 \r
- 2.26 821.14 \r
- 2.58 817.85 \r
- 2.91 801.07 \r
- 3.14 773.94 \r
- 3.25 750.13 \r
- 3.32 743.39 \r
- 3.37 729.83 \r
- 3.42 688.83 \r
- 3.46 593.37 \r
- 3.50 484.14 \r
- 3.53 368.18 \r
- 3.57 248.80 \r
- 3.62 149.82 \r
- 3.66 61.13 \r
- 3.72 0.00 \r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="221.63" Itot="2593.14" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="697.081" burn-time="3.72" cgDiv="10" cgFix="1" cgStep="-1." code="L700BB" delays="1000" dia="75." exitDia="0." initWt="2732." len="368." mDiv="10" mFix="1" mStep="-1." massFrac="43.67" mfg="Animal Motor Works" peakThrust="821.14" propWt="1193.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="184." f="0." m="1193.1" t="0."/>\r
+<eng-data cg="184." f="221.87" m="1192.08" t="0.02"/>\r
+<eng-data cg="184." f="399.33" m="1190.65" t="0.03"/>\r
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+<eng-data cg="184." f="494.89" m="1180.02" t="0.08"/>\r
+<eng-data cg="184." f="498.41" m="1168.59" t="0.13"/>\r
+<eng-data cg="184." f="535.99" m="1142.42" t="0.24"/>\r
+<eng-data cg="184." f="614.67" m="1078.89" t="0.48"/>\r
+<eng-data cg="184." f="683.2" m="992.302" t="0.77"/>\r
+<eng-data cg="184." f="755.25" m="840.081" t="1.23"/>\r
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+<eng-data cg="184." f="801.07" m="219.861" t="2.91"/>\r
+<eng-data cg="184." f="773.94" m="136.525" t="3.14"/>\r
+<eng-data cg="184." f="750.13" m="97.9582" t="3.25"/>\r
+<eng-data cg="184." f="743.39" m="73.9074" t="3.32"/>\r
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+<eng-data cg="184." f="688.83" m="40.6437" t="3.42"/>\r
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+<eng-data cg="184." f="484.14" m="18.9297" t="3.5"/>\r
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+<eng-data cg="184." f="248.8" m="7.37004" t="3.57"/>\r
+<eng-data cg="184." f="149.82" m="2.78493" t="3.62"/>\r
+<eng-data cg="184." f="61.13" m="0.843774" t="3.66"/>\r
+<eng-data cg="184." f="0." m="0." t="3.72"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="181.49" Itot="3136.62" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="774.475" burn-time="4.05" cgDiv="10" cgFix="1" cgStep="-1." code="L777WW" delays="1000" dia="75." exitDia="0." initWt="3698.7" len="497." mDiv="10" mFix="1" mStep="-1." massFrac="47.65" mfg="Animal Motor Works" peakThrust="1000.16" propWt="1762.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW L777 RASP.ENG file made from NAR published data\r
+File produced SEPT 4, 2002\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="248.5" f="0." m="1762.3" t="0."/>\r
+<eng-data cg="248.5" f="140.882" m="1761.31" t="0.025"/>\r
+<eng-data cg="248.5" f="209.474" m="1757.47" t="0.064"/>\r
+<eng-data cg="248.5" f="360.055" m="1750.43" t="0.108"/>\r
+<eng-data cg="248.5" f="652.185" m="1723.13" t="0.204"/>\r
+<eng-data cg="248.5" f="641.518" m="1666.44" t="0.36"/>\r
+<eng-data cg="248.5" f="693.745" m="1661.56" t="0.373"/>\r
+<eng-data cg="248.5" f="683.28" m="1644.15" t="0.418"/>\r
+<eng-data cg="248.5" f="730.073" m="1600.48" t="0.528"/>\r
+<eng-data cg="248.5" f="761.268" m="1540.99" t="0.67"/>\r
+<eng-data cg="248.5" f="781.998" m="1501.54" t="0.761"/>\r
+<eng-data cg="248.5" f="802.828" m="1489.96" t="0.787"/>\r
+<eng-data cg="248.5" f="802.728" m="1452.07" t="0.871"/>\r
+<eng-data cg="248.5" f="854.754" m="1361.74" t="1.065"/>\r
+<eng-data cg="248.5" f="911.811" m="1226.26" t="1.338"/>\r
+<eng-data cg="248.5" f="963.636" m="1052.4" t="1.668"/>\r
+<eng-data cg="248.5" f="989.498" m="917.423" t="1.914"/>\r
+<eng-data cg="248.5" f="1000.16" m="805.075" t="2.115"/>\r
+<eng-data cg="248.5" f="962.831" m="665.559" t="2.368"/>\r
+<eng-data cg="248.5" f="926." m="517.517" t="2.647"/>\r
+<eng-data cg="248.5" f="878.603" m="346.166" t="2.985"/>\r
+<eng-data cg="248.5" f="805.143" m="195.751" t="3.303"/>\r
+<eng-data cg="248.5" f="752.815" m="121.785" t="3.472"/>\r
+<eng-data cg="248.5" f="705.72" m="89.8257" t="3.55"/>\r
+<eng-data cg="248.5" f="648.26" m="70.0468" t="3.602"/>\r
+<eng-data cg="248.5" f="611.631" m="54.1198" t="3.647"/>\r
+<eng-data cg="248.5" f="512.409" m="39.5944" t="3.693"/>\r
+<eng-data cg="248.5" f="334.897" m="19.124" t="3.779"/>\r
+<eng-data cg="248.5" f="178.216" m="7.8807" t="3.857"/>\r
+<eng-data cg="248.5" f="89.379" m="2.01715" t="3.935"/>\r
+<eng-data cg="248.5" f="26.687" m="0.517293" t="3.981"/>\r
+<eng-data cg="248.5" f="0." m="0." t="4.05"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works L777 White Wolf\r
-L777WW 75 497 0 1.7623 3.6987 AMW\r
-0.025 140.882\r
-0.064 209.474\r
-0.108 360.055\r
-0.204 652.185\r
-0.360 641.518\r
-0.373 693.745\r
-0.418 683.28\r
-0.528 730.073\r
-0.670 761.268\r
-0.761 781.998\r
-0.787 802.828\r
-0.871 802.728\r
-1.065 854.754\r
-1.338 911.811\r
-1.668 963.636\r
-1.914 989.498\r
-2.115 1000.16\r
-2.368 962.831\r
-2.647 926\r
-2.985 878.603\r
-3.303 805.143\r
-3.472 752.815\r
-3.550 705.72\r
-3.602 648.26\r
-3.647 611.631\r
-3.693 512.409\r
-3.779 334.897\r
-3.857 178.216\r
-3.935 89.379\r
-3.981 26.687\r
-4.050 0\r
+++ /dev/null
-;\r
-;AMW L900 RASP.ENG file made from NAR published data\r
-;File produced April 19, 2004\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-L900RR 75 497 100 1.771 3.5888 Animal_Motor_Works \r
-0.029 464.292\r
-0.053 630.937\r
-0.059 684.506\r
-0.096 702.328\r
-0.133 696.387\r
-0.201 714.311\r
-0.486 803.524\r
-0.777 910.661\r
-1.099 988.093\r
-1.26 1041.16\r
-1.284 1071.37\r
-1.378 1053.24\r
-1.607 1101.57\r
-1.917 1142.86\r
-2.208 1173.56\r
-2.413 1160.98\r
-2.624 1107.62\r
-2.866 976.211\r
-3.053 886.897\r
-3.208 839.27\r
-3.314 827.388\r
-3.382 809.465\r
-3.432 720.252\r
-3.495 547.564\r
-3.57 345.273\r
-3.627 214.273\r
-3.714 77.382\r
-3.79 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="198.12" Itot="3440.91" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="907.891" burn-time="3.79" cgDiv="10" cgFix="1" cgStep="-1." code="L900RR" delays="1000" dia="75." exitDia="0." initWt="3588.8" len="497." mDiv="10" mFix="1" mStep="-1." massFrac="49.35" mfg="Animal Motor Works" peakThrust="1173.56" propWt="1771." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW L900 RASP.ENG file made from NAR published data\r
+File produced April 19, 2004\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="248.5" f="0." m="1771." t="0."/>\r
+<eng-data cg="248.5" f="464.292" m="1767.53" t="0.029"/>\r
+<eng-data cg="248.5" f="630.937" m="1760.77" t="0.053"/>\r
+<eng-data cg="248.5" f="684.506" m="1758.74" t="0.059"/>\r
+<eng-data cg="248.5" f="702.328" m="1745.53" t="0.096"/>\r
+<eng-data cg="248.5" f="696.387" m="1732.22" t="0.133"/>\r
+<eng-data cg="248.5" f="714.311" m="1707.53" t="0.201"/>\r
+<eng-data cg="248.5" f="803.524" m="1596.21" t="0.486"/>\r
+<eng-data cg="248.5" f="910.661" m="1467.84" t="0.777"/>\r
+<eng-data cg="248.5" f="988.093" m="1310.5" t="1.099"/>\r
+<eng-data cg="248.5" f="1041.16" m="1226.42" t="1.26"/>\r
+<eng-data cg="248.5" f="1071.37" m="1213.37" t="1.284"/>\r
+<eng-data cg="248.5" f="1053.24" m="1161.98" t="1.378"/>\r
+<eng-data cg="248.5" f="1101.57" m="1034.99" t="1.607"/>\r
+<eng-data cg="248.5" f="1142.86" m="855.934" t="1.917"/>\r
+<eng-data cg="248.5" f="1173.56" m="682.464" t="2.208"/>\r
+<eng-data cg="248.5" f="1160.98" m="559.303" t="2.413"/>\r
+<eng-data cg="248.5" f="1107.62" m="436.119" t="2.624"/>\r
+<eng-data cg="248.5" f="976.211" m="306.343" t="2.866"/>\r
+<eng-data cg="248.5" f="886.897" m="216.684" t="3.053"/>\r
+<eng-data cg="248.5" f="839.27" m="147.83" t="3.208"/>\r
+<eng-data cg="248.5" f="827.388" m="102.366" t="3.314"/>\r
+<eng-data cg="248.5" f="809.465" m="73.7217" t="3.382"/>\r
+<eng-data cg="248.5" f="720.252" m="54.0384" t="3.432"/>\r
+<eng-data cg="248.5" f="547.564" m="33.4836" t="3.495"/>\r
+<eng-data cg="248.5" f="345.273" m="16.2511" t="3.57"/>\r
+<eng-data cg="248.5" f="214.273" m="8.04332" t="3.627"/>\r
+<eng-data cg="248.5" f="77.382" m="1.51345" t="3.714"/>\r
+<eng-data cg="248.5" f="0." m="0." t="3.79"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works M1350 White Wolf\r
-M1350WW 75 781 0 2.92700 5.40300 AMW\r
-0.03 1197.771588\r
-0.04 1465.181058\r
-0.07 1660.167131\r
-0.09 1665.738162\r
-0.16 1587.743733\r
-0.45 1587.743733\r
-0.61 1576.601671\r
-1.86 1649.02507\r
-2.27 1643.454039\r
-2.64 1598.885794\r
-3.18 1504.178273\r
-3.29 1353.760446\r
-3.41 991.643454\r
-3.49 841.2256267\r
-3.62 646.2395543\r
-3.74 428.9693593\r
-3.90 373.2590529\r
-4.22 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="196.24" Itot="5710.57" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1350.02" burn-time="4.23" cgDiv="10" cgFix="1" cgStep="-1." code="M1350WW" delays="1000" dia="75." exitDia="0." initWt="5632.2" len="785." mDiv="10" mFix="1" mStep="-1." massFrac="52.68" mfg="Animal Motor Works" peakThrust="1662.71" propWt="2967.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Animal Motor Works M1350 RASP.ENG file made from NAR data\r
+File produced Nov 3, 2002\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="392.5" f="0." m="2967.3" t="0."/>\r
+<eng-data cg="392.5" f="728.705" m="2962.38" t="0.026"/>\r
+<eng-data cg="392.5" f="1381.7" m="2951.41" t="0.046"/>\r
+<eng-data cg="392.5" f="1609.64" m="2935.87" t="0.066"/>\r
+<eng-data cg="392.5" f="1662.71" m="2913.76" t="0.092"/>\r
+<eng-data cg="392.5" f="1609.64" m="2863.6" t="0.151"/>\r
+<eng-data cg="392.5" f="1592.57" m="2787.89" t="0.242"/>\r
+<eng-data cg="392.5" f="1592.57" m="2592.6" t="0.478"/>\r
+<eng-data cg="392.5" f="1592.57" m="2126.7" t="1.041"/>\r
+<eng-data cg="392.5" f="1635.75" m="1565.58" t="1.71"/>\r
+<eng-data cg="392.5" f="1643.78" m="1063.73" t="2.299"/>\r
+<eng-data cg="392.5" f="1601.61" m="749.223" t="2.672"/>\r
+<eng-data cg="392.5" f="1508.22" m="409.881" t="3.092"/>\r
+<eng-data cg="392.5" f="1500.19" m="327.812" t="3.197"/>\r
+<eng-data cg="392.5" f="1423.87" m="288.308" t="3.249"/>\r
+<eng-data cg="392.5" f="1338.52" m="250.988" t="3.301"/>\r
+<eng-data cg="392.5" f="1067.4" m="197.856" t="3.386"/>\r
+<eng-data cg="392.5" f="788.05" m="131.332" t="3.524"/>\r
+<eng-data cg="392.5" f="440.617" m="68.4463" t="3.721"/>\r
+<eng-data cg="392.5" f="389.807" m="55.9328" t="3.779"/>\r
+<eng-data cg="392.5" f="381.272" m="44.1132" t="3.838"/>\r
+<eng-data cg="392.5" f="364.402" m="31.3269" t="3.904"/>\r
+<eng-data cg="392.5" f="305.058" m="18.8039" t="3.976"/>\r
+<eng-data cg="392.5" f="194.903" m="8.54227" t="4.055"/>\r
+<eng-data cg="392.5" f="93.214" m="2.17959" t="4.14"/>\r
+<eng-data cg="392.5" f="0." m="0." t="4.23"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;AMW M1480 RASP.ENG file made from NAR published data\r
-;File produced April 19, 2004\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-M1480RR 75 785 100 3 5.5248 Animal_Motor_Works \r
-0.022 713.002\r
-0.032 1254.68\r
-0.055 1473.37\r
-0.078 1569.11\r
-0.156 1569.11\r
-0.352 1559.03\r
-0.642 1597.33\r
-0.974 1644.69\r
-1.289 1702.13\r
-1.52 1739.42\r
-1.918 1796.87\r
-2.279 1814.83\r
-2.481 1796.87\r
-2.707 1739.42\r
-2.968 1644.69\r
-3.058 1616.47\r
-3.135 1520.73\r
-3.218 1378.64\r
-3.284 1217.39\r
-3.332 1065.22\r
-3.344 1140.8\r
-3.368 1016.85\r
-3.41 741.522\r
-3.5 522.935\r
-3.613 275.727\r
-3.691 171.12\r
-3.768 66.553\r
-3.85 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="194.79" Itot="5730.8" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1488.52" burn-time="3.85" cgDiv="10" cgFix="1" cgStep="-1." code="M1480RR" delays="1000" dia="75." exitDia="0." initWt="5524.8" len="785." mDiv="10" mFix="1" mStep="-1." massFrac="54.3" mfg="Animal Motor Works" peakThrust="1814.83" propWt="3000." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW M1480 RASP.ENG file made from NAR published data\r
+File produced April 19, 2004\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="392.5" f="0." m="3000." t="0."/>\r
+<eng-data cg="392.5" f="713.002" m="2995.89" t="0.022"/>\r
+<eng-data cg="392.5" f="1254.68" m="2990.74" t="0.032"/>\r
+<eng-data cg="392.5" f="1473.37" m="2974.32" t="0.055"/>\r
+<eng-data cg="392.5" f="1569.11" m="2956." t="0.078"/>\r
+<eng-data cg="392.5" f="1569.11" m="2891.93" t="0.156"/>\r
+<eng-data cg="392.5" f="1559.03" m="2731.46" t="0.352"/>\r
+<eng-data cg="392.5" f="1597.33" m="2491.87" t="0.642"/>\r
+<eng-data cg="392.5" f="1644.69" m="2210.14" t="0.974"/>\r
+<eng-data cg="392.5" f="1702.13" m="1934.2" t="1.289"/>\r
+<eng-data cg="392.5" f="1739.42" m="1726.11" t="1.52"/>\r
+<eng-data cg="392.5" f="1796.87" m="1357.72" t="1.918"/>\r
+<eng-data cg="392.5" f="1814.83" m="1016.46" t="2.279"/>\r
+<eng-data cg="392.5" f="1796.87" m="825.498" t="2.481"/>\r
+<eng-data cg="392.5" f="1739.42" m="616.313" t="2.707"/>\r
+<eng-data cg="392.5" f="1644.69" m="385.127" t="2.968"/>\r
+<eng-data cg="392.5" f="1616.47" m="308.304" t="3.058"/>\r
+<eng-data cg="392.5" f="1520.73" m="245.076" t="3.135"/>\r
+<eng-data cg="392.5" f="1378.64" m="182.088" t="3.218"/>\r
+<eng-data cg="392.5" f="1217.39" m="137.241" t="3.284"/>\r
+<eng-data cg="392.5" f="1065.22" m="108.563" t="3.332"/>\r
+<eng-data cg="392.5" f="1140.8" m="101.634" t="3.344"/>\r
+<eng-data cg="392.5" f="1016.85" m="88.0803" t="3.368"/>\r
+<eng-data cg="392.5" f="741.522" m="68.7501" t="3.41"/>\r
+<eng-data cg="392.5" f="522.935" m="38.9634" t="3.5"/>\r
+<eng-data cg="392.5" f="275.727" m="15.3414" t="3.613"/>\r
+<eng-data cg="392.5" f="171.12" m="6.21855" t="3.691"/>\r
+<eng-data cg="392.5" f="66.553" m="1.42843" t="3.768"/>\r
+<eng-data cg="392.5" f="0." m="0." t="3.85"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works 98-11000\r
-M1730SK 98 870 0 4.9452 9.8718 AMW\r
-0.040 682.642\r
-0.064 1153.387\r
-0.221 1354.665\r
-0.269 1414.771\r
-0.381 1458.026\r
-0.541 1526.924\r
-0.701 1589.200\r
-0.861 1675.203\r
-1.021 1732.669\r
-1.181 1802.227\r
-1.341 1886.644\r
-1.500 1973.713\r
-1.660 2070.514\r
-1.820 2183.822\r
-1.980 2299.313\r
-2.140 2433.862\r
-2.300 2568.119\r
-2.460 2679.423\r
-2.620 2638.376\r
-2.780 2484.185\r
-2.940 2306.038\r
-3.099 2173.849\r
-3.259 2074.688\r
-3.419 1961.303\r
-3.579 1807.810\r
-3.739 1640.258\r
-3.899 1303.035\r
-4.059 940.600\r
-4.219 567.152\r
-4.379 309.143\r
-4.539 188.981\r
-4.637 0.000\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="166.23" Itot="8061.6" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1737.41" burn-time="4.64" cgDiv="10" cgFix="1" cgStep="-1." code="M1730SK" delays="1000" dia="98." exitDia="0." initWt="9871.8" len="870." mDiv="10" mFix="1" mStep="-1." massFrac="50.09" mfg="Animal Motor Works" peakThrust="2679.42" propWt="4945.2" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="435." f="0." m="4945.2" t="0."/>\r
+<eng-data cg="435." f="682.64" m="4936.83" t="0.04"/>\r
+<eng-data cg="435." f="1153.39" m="4925.56" t="0.06"/>\r
+<eng-data cg="435." f="1354.67" m="4802.48" t="0.22"/>\r
+<eng-data cg="435." f="1414.77" m="4760.01" t="0.27"/>\r
+<eng-data cg="435." f="1458.03" m="4663.09" t="0.38"/>\r
+<eng-data cg="435." f="1526.92" m="4516.6" t="0.54"/>\r
+<eng-data cg="435." f="1589.2" m="4363.68" t="0.7"/>\r
+<eng-data cg="435." f="1675.2" m="4203.48" t="0.86"/>\r
+<eng-data cg="435." f="1732.67" m="4036.25" t="1.02"/>\r
+<eng-data cg="435." f="1802.23" m="3862.77" t="1.18"/>\r
+<eng-data cg="435." f="1886.64" m="3681.74" t="1.34"/>\r
+<eng-data cg="435." f="1973.71" m="3492.3" t="1.5"/>\r
+<eng-data cg="435." f="2070.51" m="3293.83" t="1.66"/>\r
+<eng-data cg="435." f="2183.82" m="3085.06" t="1.82"/>\r
+<eng-data cg="435." f="2299.31" m="2865.05" t="1.98"/>\r
+<eng-data cg="435." f="2433.86" m="2632.78" t="2.14"/>\r
+<eng-data cg="435." f="2568.12" m="2387.31" t="2.3"/>\r
+<eng-data cg="435." f="2679.42" m="2129.79" t="2.46"/>\r
+<eng-data cg="435." f="2638.38" m="1868.82" t="2.62"/>\r
+<eng-data cg="435." f="2484.18" m="1617.44" t="2.78"/>\r
+<eng-data cg="435." f="2306.04" m="1382.36" t="2.94"/>\r
+<eng-data cg="435." f="2173.85" m="1162.51" t="3.1"/>\r
+<eng-data cg="435." f="2074.69" m="954.02" t="3.26"/>\r
+<eng-data cg="435." f="1961.3" m="755.958" t="3.42"/>\r
+<eng-data cg="435." f="1807.81" m="570.992" t="3.58"/>\r
+<eng-data cg="435." f="1640.26" m="401.781" t="3.74"/>\r
+<eng-data cg="435." f="1303.04" m="257.341" t="3.9"/>\r
+<eng-data cg="435." f="940.6" m="147.236" t="4.06"/>\r
+<eng-data cg="435." f="567.15" m="73.2443" t="4.22"/>\r
+<eng-data cg="435." f="309.14" m="30.2411" t="4.38"/>\r
+<eng-data cg="435." f="188.98" m="5.79627" t="4.54"/>\r
+<eng-data cg="435." f="0." m="0." t="4.64"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; Animal Motor Works M1850GG\r
-; estimated from TRA graph by John DeMar jsdemar@syr.edu\r
-; motor mass is a guess based on similar types\r
-M1850GG 75 781 0 3.3750 4.5000 AMW\r
- 0.08 979.00 \r
- 0.13 1180.00 \r
- 0.28 1290.00 \r
- 0.33 1468.00 \r
- 0.73 1936.00 \r
- 1.33 2202.00 \r
- 1.73 2279.00 \r
- 2.58 2105.00 \r
- 2.83 2007.00 \r
- 2.88 1860.00 \r
- 3.08 538.00 \r
- 3.20 174.00 \r
- 3.30 0.00 \r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="177.25" Itot="5866.36" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1833.24" burn-time="3.2" cgDiv="10" cgFix="1" cgStep="-1." code="M1850GG" delays="1000" dia="76." exitDia="0." initWt="5851." len="781." mDiv="10" mFix="1" mStep="-1." massFrac="57.68" mfg="Animal Motor Works" peakThrust="2312.19" propWt="3375." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>M1850GG entered by Tim Van Milligan\r
+For RockSim - http://www.rocksim.com\r
+Based on TRA Certification paperwork from 06-01-2002\r
+Initial Mass from Jim Robinson at AMW\r
+Not approved by TRA or AMW.\r
+</comments>\r
+<data>\r
+<eng-data cg="390.5" f="0." m="3375." t="0."/>\r
+<eng-data cg="390.5" f="902.857" m="3366.95" t="0.031"/>\r
+<eng-data cg="390.5" f="1068.01" m="3344.84" t="0.07"/>\r
+<eng-data cg="390.5" f="1101.05" m="3282.44" t="0.17"/>\r
+<eng-data cg="390.5" f="1288.22" m="3224.02" t="0.255"/>\r
+<eng-data cg="390.5" f="1420.35" m="3201.43" t="0.284"/>\r
+<eng-data cg="390.5" f="1464.39" m="3122.6" t="0.379"/>\r
+<eng-data cg="390.5" f="1497.42" m="3083.41" t="0.425"/>\r
+<eng-data cg="390.5" f="1673.59" m="3013.17" t="0.502"/>\r
+<eng-data cg="390.5" f="1695.61" m="2960.83" t="0.556"/>\r
+<eng-data cg="390.5" f="1871.78" m="2848.98" t="0.665"/>\r
+<eng-data cg="390.5" f="1893.8" m="2731.99" t="0.773"/>\r
+<eng-data cg="390.5" f="2069.96" m="2485.71" t="0.989"/>\r
+<eng-data cg="390.5" f="2180.07" m="2173.96" t="1.244"/>\r
+<eng-data cg="390.5" f="2268.15" m="1866.87" t="1.484"/>\r
+<eng-data cg="390.5" f="2312.19" m="1520.35" t="1.747"/>\r
+<eng-data cg="390.5" f="2268.15" m="1194.91" t="1.994"/>\r
+<eng-data cg="390.5" f="2224.11" m="835.668" t="2.272"/>\r
+<eng-data cg="390.5" f="2136.03" m="476.959" t="2.558"/>\r
+<eng-data cg="390.5" f="2003.9" m="247.12" t="2.751"/>\r
+<eng-data cg="390.5" f="1981.88" m="202.405" t="2.79"/>\r
+<eng-data cg="390.5" f="1783.69" m="135.247" t="2.852"/>\r
+<eng-data cg="390.5" f="770.732" m="27.9666" t="2.998"/>\r
+<eng-data cg="390.5" f="330.314" m="8.3298" t="3.06"/>\r
+<eng-data cg="390.5" f="44.041" m="0.899477" t="3.129"/>\r
+<eng-data cg="390.5" f="0." m="0." t="3.2"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works M1850 Green Gorilla\r
-M1850GG 75 781 0 3.37000 5.85100 AMW\r
-0.12 1201.01994\r
-0.25 1321.121934\r
-0.37 1579.11881\r
-0.50 1699.220804\r
-0.62 1846.01213\r
-0.75 1930.528348\r
-0.87 1997.251678\r
-1.00 2059.526786\r
-1.12 2126.250116\r
-1.25 2192.973446\r
-1.37 2224.111\r
-1.50 2246.35211\r
-1.62 2268.59322\r
-1.75 2277.489664\r
-1.87 2268.59322\r
-2.00 2246.35211\r
-2.12 2224.111\r
-2.25 2192.973446\r
-2.37 2166.284114\r
-2.50 2144.043004\r
-2.62 2099.560784\r
-2.75 2046.18212\r
-2.87 1912.73546\r
-3.00 831.817514\r
-3.12 311.37554\r
-3.25 84.516218\r
-3.3 0.000\r
+++ /dev/null
-;\r
-;AMW M1900 RASP.ENG file made from NAR published data\r
-;File produced April 19, 2004\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-M1900BB 75 785 100 2.733 5.4225 Animal_Motor_Works \r
-0.018 1109.21\r
-0.044 1761.75\r
-0.061 1910.65\r
-0.085 1938.62\r
-0.159 1929.63\r
-0.29 1956.62\r
-0.409 2031.56\r
-0.438 1974.6\r
-0.569 2011.58\r
-0.815 2104.51\r
-1.073 2197.44\r
-1.401 2280.39\r
-1.688 2324.7\r
-1.905 2297.37\r
-2.073 2241.41\r
-2.254 2138.49\r
-2.397 2063.54\r
-2.479 2016.57\r
-2.54 2025.57\r
-2.581 2006.58\r
-2.63 1885.67\r
-2.716 1493.94\r
-2.805 1120.21\r
-2.887 840.605\r
-2.972 569.996\r
-3.046 299.488\r
-3.119 150.193\r
-3.168 56.829\r
-3.23 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="225.39" Itot="6040.88" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1870.24" burn-time="3.23" cgDiv="10" cgFix="1" cgStep="-1." code="M1900BB" delays="1000" dia="75." exitDia="0." initWt="5422.5" len="785." mDiv="10" mFix="1" mStep="-1." massFrac="50.4" mfg="Animal Motor Works" peakThrust="2324.7" propWt="2733." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW M1900 RASP.ENG file made from NAR published data\r
+File produced April 19, 2004\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="392.5" f="0." m="2733." t="0."/>\r
+<eng-data cg="392.5" f="1109.21" m="2728.48" t="0.018"/>\r
+<eng-data cg="392.5" f="1761.75" m="2711.6" t="0.044"/>\r
+<eng-data cg="392.5" f="1910.65" m="2697.48" t="0.061"/>\r
+<eng-data cg="392.5" f="1938.62" m="2676.58" t="0.085"/>\r
+<eng-data cg="392.5" f="1929.63" m="2611.83" t="0.159"/>\r
+<eng-data cg="392.5" f="1956.62" m="2496.66" t="0.29"/>\r
+<eng-data cg="392.5" f="2031.56" m="2389.31" t="0.409"/>\r
+<eng-data cg="392.5" f="1974.6" m="2363.02" t="0.438"/>\r
+<eng-data cg="392.5" f="2011.58" m="2244.9" t="0.569"/>\r
+<eng-data cg="392.5" f="2104.51" m="2015.85" t="0.815"/>\r
+<eng-data cg="392.5" f="2197.44" m="1764.78" t="1.073"/>\r
+<eng-data cg="392.5" f="2280.39" m="1432.54" t="1.401"/>\r
+<eng-data cg="392.5" f="2324.7" m="1133.57" t="1.688"/>\r
+<eng-data cg="392.5" f="2297.37" m="906.685" t="1.905"/>\r
+<eng-data cg="392.5" f="2241.41" m="734.197" t="2.073"/>\r
+<eng-data cg="392.5" f="2138.49" m="554.868" t="2.254"/>\r
+<eng-data cg="392.5" f="2063.54" m="418.941" t="2.397"/>\r
+<eng-data cg="392.5" f="2016.57" m="343.258" t="2.479"/>\r
+<eng-data cg="392.5" f="2025.57" m="287.482" t="2.54"/>\r
+<eng-data cg="392.5" f="2006.58" m="250.085" t="2.581"/>\r
+<eng-data cg="392.5" f="1885.67" m="206.943" t="2.63"/>\r
+<eng-data cg="392.5" f="1493.94" m="141.196" t="2.716"/>\r
+<eng-data cg="392.5" f="1120.21" m="88.5662" t="2.805"/>\r
+<eng-data cg="392.5" f="840.605" m="52.1948" t="2.887"/>\r
+<eng-data cg="392.5" f="569.996" m="25.0721" t="2.972"/>\r
+<eng-data cg="392.5" f="299.488" m="10.5174" t="3.046"/>\r
+<eng-data cg="392.5" f="150.193" m="3.09171" t="3.119"/>\r
+<eng-data cg="392.5" f="56.829" m="0.797024" t="3.168"/>\r
+<eng-data cg="392.5" f="0." m="0." t="3.23"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="169.92" Itot="6275.34" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2017.79" burn-time="3.11" cgDiv="10" cgFix="1" cgStep="-1." code="M2200SK" delays="1000" dia="75." exitDia="0." initWt="7009.8" len="1039." mDiv="10" mFix="1" mStep="-1." massFrac="53.72" mfg="Animal Motor Works" peakThrust="2979.38" propWt="3766." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW M2200SK RASP.ENG file made from NAR published data\r
+File produced April 19, 2004\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="519.5" f="0." m="3766." t="0."/>\r
+<eng-data cg="519.5" f="972.329" m="3760.16" t="0.02"/>\r
+<eng-data cg="519.5" f="1612.84" m="3737.67" t="0.049"/>\r
+<eng-data cg="519.5" f="1601.78" m="3687.51" t="0.101"/>\r
+<eng-data cg="519.5" f="1701.33" m="3546.77" t="0.243"/>\r
+<eng-data cg="519.5" f="1878.3" m="3290.05" t="0.482"/>\r
+<eng-data cg="519.5" f="1889.36" m="3189.44" t="0.571"/>\r
+<eng-data cg="519.5" f="2088.45" m="2913.72" t="0.802"/>\r
+<eng-data cg="519.5" f="2254.36" m="2659.61" t="0.997"/>\r
+<eng-data cg="519.5" f="2254.36" m="2556.79" t="1.073"/>\r
+<eng-data cg="519.5" f="2486.63" m="2337.71" t="1.227"/>\r
+<eng-data cg="519.5" f="2574.11" m="2035.52" t="1.426"/>\r
+<eng-data cg="519.5" f="2651.53" m="1737.59" t="1.616"/>\r
+<eng-data cg="519.5" f="2751.08" m="1632.22" t="1.681"/>\r
+<eng-data cg="519.5" f="2839.56" m="1462.79" t="1.782"/>\r
+<eng-data cg="519.5" f="2817.44" m="1379.61" t="1.831"/>\r
+<eng-data cg="519.5" f="2916.99" m="1155.92" t="1.961"/>\r
+<eng-data cg="519.5" f="2979.38" m="963.069" t="2.07"/>\r
+<eng-data cg="519.5" f="2939.11" m="812.115" t="2.155"/>\r
+<eng-data cg="519.5" f="2961.23" m="739.526" t="2.196"/>\r
+<eng-data cg="519.5" f="2872.75" m="634.492" t="2.256"/>\r
+<eng-data cg="519.5" f="2839.56" m="523.078" t="2.321"/>\r
+<eng-data cg="519.5" f="2684.72" m="435.223" t="2.374"/>\r
+<eng-data cg="519.5" f="2331.78" m="362.97" t="2.422"/>\r
+<eng-data cg="519.5" f="1568.6" m="291.578" t="2.483"/>\r
+<eng-data cg="519.5" f="1215.66" m="257.325" t="2.524"/>\r
+<eng-data cg="519.5" f="1094." m="215.742" t="2.584"/>\r
+<eng-data cg="519.5" f="1060.81" m="157.55" t="2.674"/>\r
+<eng-data cg="519.5" f="961.268" m="113.257" t="2.747"/>\r
+<eng-data cg="519.5" f="740.358" m="51.4748" t="2.868"/>\r
+<eng-data cg="519.5" f="464.043" m="20.756" t="2.953"/>\r
+<eng-data cg="519.5" f="165.708" m="3.18227" t="3.046"/>\r
+<eng-data cg="519.5" f="0." m="0." t="3.11"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works M2500 Green Gorilla\r
-M2500GG 75 1039 0 4.248 7.5515 AMW\r
-0.026 1288.791\r
-0.053 2021.398\r
-0.079 2140.011\r
-0.123 2105.125\r
-0.207 2117.086\r
-0.540 2309.458\r
-0.971 2560.637\r
-1.265 2727.094\r
-1.480 2836.736\r
-1.678 2920.462\r
-1.757 2980.267\r
-1.946 2995.51\r
-2.047 2959.335\r
-2.240 2889.563\r
-2.310 2854.677\r
-2.486 2820.788\r
-2.526 2880.593\r
-2.592 2773.941\r
-2.653 2821.785\r
-2.706 2752.012\r
-2.758 2752.012\r
-2.807 2763.973\r
-2.842 2504.82\r
-2.886 2115.092\r
-2.930 1630.674\r
-2.987 1051.565\r
-3.040 437.571\r
-3.057 284.072\r
-3.079 142.434\r
-3.110 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="186.86" Itot="7784.39" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2503.02" burn-time="3.11" cgDiv="10" cgFix="1" cgStep="-1." code="M2500GG" delays="1000" dia="75." exitDia="0." initWt="7551.5" len="1039." mDiv="10" mFix="1" mStep="-1." massFrac="56.25" mfg="Animal Motor Works" peakThrust="2995.51" propWt="4248." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Animal Motor Works M2500 RASP.ENG file made from NAR data\r
+File produced DEC 25, 2002\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="519.5" f="0." m="4248." t="0."/>\r
+<eng-data cg="519.5" f="1288.79" m="4238.86" t="0.026"/>\r
+<eng-data cg="519.5" f="2021.4" m="4214.47" t="0.053"/>\r
+<eng-data cg="519.5" f="2140.01" m="4184.95" t="0.079"/>\r
+<eng-data cg="519.5" f="2105.12" m="4133.98" t="0.123"/>\r
+<eng-data cg="519.5" f="2117.09" m="4037.21" t="0.207"/>\r
+<eng-data cg="519.5" f="2309.46" m="3635.01" t="0.54"/>\r
+<eng-data cg="519.5" f="2560.64" m="3062.29" t="0.971"/>\r
+<eng-data cg="519.5" f="2727.09" m="2638.11" t="1.265"/>\r
+<eng-data cg="519.5" f="2836.74" m="2311.72" t="1.48"/>\r
+<eng-data cg="519.5" f="2920.46" m="2000.69" t="1.678"/>\r
+<eng-data cg="519.5" f="2980.27" m="1873.49" t="1.757"/>\r
+<eng-data cg="519.5" f="2995.51" m="1565.33" t="1.946"/>\r
+<eng-data cg="519.5" f="2959.34" m="1401.22" t="2.047"/>\r
+<eng-data cg="519.5" f="2889.56" m="1093.21" t="2.24"/>\r
+<eng-data cg="519.5" f="2854.68" m="983.499" t="2.31"/>\r
+<eng-data cg="519.5" f="2820.79" m="710.95" t="2.486"/>\r
+<eng-data cg="519.5" f="2880.59" m="648.725" t="2.526"/>\r
+<eng-data cg="519.5" f="2773.94" m="546.896" t="2.592"/>\r
+<eng-data cg="519.5" f="2821.78" m="453.76" t="2.653"/>\r
+<eng-data cg="519.5" f="2752.01" m="373.156" t="2.706"/>\r
+<eng-data cg="519.5" f="2752.01" m="295.063" t="2.758"/>\r
+<eng-data cg="519.5" f="2763.97" m="221.315" t="2.807"/>\r
+<eng-data cg="519.5" f="2504.82" m="170.999" t="2.842"/>\r
+<eng-data cg="519.5" f="2115.09" m="115.534" t="2.886"/>\r
+<eng-data cg="519.5" f="1630.67" m="70.5642" t="2.93"/>\r
+<eng-data cg="519.5" f="1051.57" m="28.8482" t="2.987"/>\r
+<eng-data cg="519.5" f="437.571" m="7.31338" t="3.04"/>\r
+<eng-data cg="519.5" f="284.072" m="3.96603" t="3.057"/>\r
+<eng-data cg="519.5" f="142.434" m="1.4058" t="3.079"/>\r
+<eng-data cg="519.5" f="83.497" m="0.296172" t="3.097"/>\r
+<eng-data cg="519.5" f="0." m="0." t="3.11"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; Animal Motor Works M3000ST\r
-; estimated from TRA graph by Rob Bazinet rbazinet66@hotmail.com\r
-; motor mass is a guess based on similar types\r
-M3000ST 75 1038 0 3.8190 6.72 AMW\r
- 0.032 2494.225\r
- 0.113 2621.05 \r
- 0.242 2705.6\r
- 0.355 2811.288\r
- 0.435 2895.838\r
- 0.5 2959.25\r
- 0.645 3128.35\r
- 0.75 3297.45\r
- 0.871 3382\r
- 0.968 3551.1\r
- 1.032 3656.788\r
- 1.145 3804.75\r
- 1.355 3973.85\r
- 1.452 4037.263\r
- 1.629 4079.538\r
- 1.742 4142.95\r
- 1.903 4185.225\r
- 1.935 3847.025\r
- 2.081 3424.275\r
- 2.129 2959.25\r
- 2.177 2536.5\r
- 2.194 2113.75\r
- 2.226 1691\r
- 2.274 1268.25\r
- 2.323 845.5\r
- 2.403 422.75\r
- 2.5 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="195.12" Itot="7307.5" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2923." burn-time="2.5" cgDiv="10" cgFix="1" cgStep="-1." code="M3000ST" delays="1000" dia="75." exitDia="0." initWt="7551.5" len="1038." mDiv="10" mFix="1" mStep="-1." massFrac="50.57" mfg="Animal Motor Works" peakThrust="4115." propWt="3819." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AMW M3000ST RASP.ENG file made from Tripoli published data\r
+File produced May 15, 2004\r
+This file my be used or given away. All I ask is that this header\r
+is maintained to give credit to the people who produced the data.\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="519." f="0." m="3819." t="0."/>\r
+<eng-data cg="519." f="2721.02" m="3809.05" t="0.014"/>\r
+<eng-data cg="519." f="2553.37" m="3784.24" t="0.032"/>\r
+<eng-data cg="519." f="2601.84" m="3698.02" t="0.096"/>\r
+<eng-data cg="519." f="2722.8" m="3525.49" t="0.22"/>\r
+<eng-data cg="519." f="2807.73" m="3333.29" t="0.353"/>\r
+<eng-data cg="519." f="2928.24" m="3148.93" t="0.476"/>\r
+<eng-data cg="519." f="3048.75" m="3083.33" t="0.518"/>\r
+<eng-data cg="519." f="3061.2" m="2989.13" t="0.577"/>\r
+<eng-data cg="519." f="3314.22" m="2684.27" t="0.76"/>\r
+<eng-data cg="519." f="3519.67" m="2355.69" t="0.944"/>\r
+<eng-data cg="519." f="3772.69" m="1982.2" t="1.14"/>\r
+<eng-data cg="519." f="3942.12" m="1629.42" t="1.315"/>\r
+<eng-data cg="519." f="4039.5" m="1220.63" t="1.511"/>\r
+<eng-data cg="519." f="4088.42" m="995.496" t="1.617"/>\r
+<eng-data cg="519." f="4115." m="800.427" t="1.708"/>\r
+<eng-data cg="519." f="4089.75" m="622.479" t="1.791"/>\r
+<eng-data cg="519." f="4006.15" m="525.165" t="1.837"/>\r
+<eng-data cg="519." f="3814.49" m="451.596" t="1.873"/>\r
+<eng-data cg="519." f="3359.58" m="305.374" t="1.951"/>\r
+<eng-data cg="519." f="2784.61" m="223.493" t="2.002"/>\r
+<eng-data cg="519." f="2257.66" m="157.614" t="2.052"/>\r
+<eng-data cg="519." f="1587.08" m="98.3391" t="2.111"/>\r
+<eng-data cg="519." f="1108.15" m="62.4207" t="2.162"/>\r
+<eng-data cg="519." f="629.227" m="35.6354" t="2.221"/>\r
+<eng-data cg="519." f="318.126" m="14.0985" t="2.308"/>\r
+<eng-data cg="519." f="139.052" m="3.70519" t="2.395"/>\r
+<eng-data cg="519." f="67.503" m="0.952506" t="2.446"/>\r
+<eng-data cg="519." f="0." m="0." t="2.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works 98-11000\r
-N2020WT 98 870 0 5.1609 9.9693 AMW\r
-.106 1941.344\r
-0.221 2151.149\r
-0.381 2253.406\r
-0.541 2340.792\r
-0.701 2400.847\r
-0.861 2453.821\r
-1.021 2506.314\r
-1.181 2556.306\r
-1.341 2607.251\r
-1.500 2652.790\r
-1.660 2688.660\r
-1.820 2710.675\r
-1.980 2729.797\r
-2.140 2733.895\r
-2.300 2704.255\r
-2.460 2634.582\r
-2.620 2532.160\r
-2.780 2433.380\r
-2.940 2329.740\r
-3.099 2234.246\r
-3.259 2165.804\r
-3.419 2099.684\r
-3.579 2028.350\r
-3.739 1951.013\r
-3.899 1871.316\r
-4.059 1558.113\r
-4.219 1053.376\r
-4.379 890.506\r
-4.539 636.689\r
-4.998 0.000\r
-\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="200.78" Itot="10161.8" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2033.18" burn-time="5." cgDiv="10" cgFix="1" cgStep="-1." code="N2020WT" delays="1000" dia="98." exitDia="0." initWt="9969.3" len="870." mDiv="10" mFix="1" mStep="-1." massFrac="51.77" mfg="Animal Motor Works" peakThrust="2733.89" propWt="5160.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Animal Motor Works 98-11000</comments>\r
+<data>\r
+<eng-data cg="435." f="0." m="5160.9" t="0."/>\r
+<eng-data cg="435." f="1941.34" m="5108.64" t="0.106"/>\r
+<eng-data cg="435." f="2151.15" m="4989.13" t="0.221"/>\r
+<eng-data cg="435." f="2253.41" m="4810.18" t="0.381"/>\r
+<eng-data cg="435." f="2340.79" m="4623.52" t="0.541"/>\r
+<eng-data cg="435." f="2400.85" m="4430.86" t="0.701"/>\r
+<eng-data cg="435." f="2453.82" m="4233.62" t="0.861"/>\r
+<eng-data cg="435." f="2506.31" m="4032.09" t="1.021"/>\r
+<eng-data cg="435." f="2556.31" m="3826.4" t="1.181"/>\r
+<eng-data cg="435." f="2607.25" m="3616.6" t="1.341"/>\r
+<eng-data cg="435." f="2652.79" m="3404.23" t="1.5"/>\r
+<eng-data cg="435." f="2688.66" m="3187.2" t="1.66"/>\r
+<eng-data cg="435." f="2710.68" m="2967.83" t="1.82"/>\r
+<eng-data cg="435." f="2729.8" m="2746.79" t="1.98"/>\r
+<eng-data cg="435." f="2733.89" m="2524.8" t="2.14"/>\r
+<eng-data cg="435." f="2704.26" m="2303.85" t="2.3"/>\r
+<eng-data cg="435." f="2634.58" m="2086.93" t="2.46"/>\r
+<eng-data cg="435." f="2532.16" m="1877.01" t="2.62"/>\r
+<eng-data cg="435." f="2433.38" m="1675.26" t="2.78"/>\r
+<eng-data cg="435." f="2329.74" m="1481.73" t="2.94"/>\r
+<eng-data cg="435." f="2234.25" m="1297.46" t="3.099"/>\r
+<eng-data cg="435." f="2165.8" m="1118.69" t="3.259"/>\r
+<eng-data cg="435." f="2099.68" m="945.382" t="3.419"/>\r
+<eng-data cg="435." f="2028.35" m="777.661" t="3.579"/>\r
+<eng-data cg="435." f="1951.01" m="615.981" t="3.739"/>\r
+<eng-data cg="435." f="1871.32" m="460.68" t="3.899"/>\r
+<eng-data cg="435." f="1558.11" m="321.344" t="4.059"/>\r
+<eng-data cg="435." f="1053.38" m="215.239" t="4.219"/>\r
+<eng-data cg="435." f="890.506" m="136.26" t="4.379"/>\r
+<eng-data cg="435." f="636.689" m="74.2103" t="4.539"/>\r
+<eng-data cg="435." f="0." m="0." t="4.998"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works 98-11000\r
-N2600GG 98 870 1000 4.8812 10.4726 Animal_Motor_Works \r
-0.024 1674.37\r
-0.064 1949.62\r
-0.104 2039.52\r
-0.306 2189.98\r
-0.508 2334.45\r
-0.709 2491.23\r
-0.911 2668.93\r
-1.113 2874.7\r
-1.314 3038.83\r
-1.516 3191.29\r
-1.718 3266.01\r
-1.92 3318.98\r
-2.121 3336.18\r
-2.323 3229.26\r
-2.525 3089.68\r
-2.726 2943.98\r
-2.928 2847.69\r
-3.13 2751.68\r
-3.331 2682.22\r
-3.533 2463.48\r
-3.735 1339.63\r
-3.937 269.834\r
-4.034 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="219.69" Itot="10516." Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2606.84" burn-time="4.03" cgDiv="10" cgFix="1" cgStep="-1." code="N2600GG" delays="1000" dia="98." exitDia="0." initWt="10472.6" len="870." mDiv="10" mFix="1" mStep="-1." massFrac="46.61" mfg="Animal Motor Works" peakThrust="3336.18" propWt="4881.2" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Animal Motor Works 98-11000</comments>\r
+<data>\r
+<eng-data cg="435." f="0." m="4881.2" t="0."/>\r
+<eng-data cg="435." f="1674.37" m="4871.87" t="0.024"/>\r
+<eng-data cg="435." f="1949.62" m="4838.23" t="0.064"/>\r
+<eng-data cg="435." f="2039.52" m="4801.2" t="0.104"/>\r
+<eng-data cg="435." f="2189.98" m="4602.92" t="0.306"/>\r
+<eng-data cg="435." f="2334.45" m="4390.81" t="0.508"/>\r
+<eng-data cg="435." f="2491.23" m="4165.69" t="0.709"/>\r
+<eng-data cg="435." f="2668.93" m="3923.78" t="0.911"/>\r
+<eng-data cg="435." f="2874.7" m="3663.89" t="1.113"/>\r
+<eng-data cg="435." f="3038.83" m="3388.03" t="1.314"/>\r
+<eng-data cg="435." f="3191.29" m="3095.95" t="1.516"/>\r
+<eng-data cg="435." f="3266.01" m="2793.23" t="1.718"/>\r
+<eng-data cg="435." f="3318.98" m="2484.52" t="1.92"/>\r
+<eng-data cg="435." f="3336.18" m="2174.06" t="2.121"/>\r
+<eng-data cg="435." f="3229.26" m="1866.27" t="2.323"/>\r
+<eng-data cg="435." f="3089.68" m="1570.03" t="2.525"/>\r
+<eng-data cg="435." f="2943.98" m="1288.57" t="2.726"/>\r
+<eng-data cg="435." f="2847.69" m="1017.05" t="2.928"/>\r
+<eng-data cg="435." f="2751.68" m="754.543" t="3.13"/>\r
+<eng-data cg="435." f="2682.22" m="501.057" t="3.331"/>\r
+<eng-data cg="435." f="2463.48" m="259.821" t="3.533"/>\r
+<eng-data cg="435." f="1339.63" m="81.5278" t="3.735"/>\r
+<eng-data cg="435." f="269.834" m="6.07455" t="3.937"/>\r
+<eng-data cg="435." f="0." m="0." t="4.034"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works 98-11000\r
-N2700BB 98 870 1000 4.7837 9.9308 Animal_Motor_Works \r
-0.027 2229.53\r
-0.069 2476.18\r
-0.111 2539.74\r
-0.36 2723.21\r
-0.527 2863.83\r
-0.735 3016.48\r
-0.943 3141.25\r
-1.151 3241.72\r
-1.359 3335.56\r
-1.567 3519.92\r
-1.775 3425.88\r
-1.983 3420.56\r
-2.191 3356.08\r
-2.399 3270.48\r
-2.607 3182.6\r
-2.815 3098.31\r
-3.023 3002.95\r
-3.231 2888.73\r
-3.439 2266.61\r
-3.647 1498.26\r
-3.855 780.04\r
-4.063 233.545\r
-4.16 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="241.94" Itot="11350.1" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2728.39" burn-time="4.16" cgDiv="10" cgFix="1" cgStep="-1." code="N2700BB" delays="1000" dia="98." exitDia="0." initWt="9930.8" len="870." mDiv="10" mFix="1" mStep="-1." massFrac="48.17" mfg="Animal Motor Works" peakThrust="3519.92" propWt="4783.7" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Animal Motor Works 98-11000</comments>\r
+<data>\r
+<eng-data cg="435." f="0." m="4783.7" t="0."/>\r
+<eng-data cg="435." f="2229.53" m="4771.01" t="0.027"/>\r
+<eng-data cg="435." f="2476.18" m="4729.37" t="0.069"/>\r
+<eng-data cg="435." f="2539.74" m="4684.97" t="0.111"/>\r
+<eng-data cg="435." f="2723.21" m="4408.81" t="0.36"/>\r
+<eng-data cg="435." f="2863.83" m="4212.19" t="0.527"/>\r
+<eng-data cg="435." f="3016.48" m="3954.44" t="0.735"/>\r
+<eng-data cg="435." f="3141.25" m="3684.53" t="0.943"/>\r
+<eng-data cg="435." f="3241.72" m="3404.75" t="1.151"/>\r
+<eng-data cg="435." f="3335.56" m="3116.45" t="1.359"/>\r
+<eng-data cg="435." f="3519.92" m="2815.95" t="1.567"/>\r
+<eng-data cg="435." f="3425.88" m="2511.5" t="1.775"/>\r
+<eng-data cg="435." f="3420.56" m="2211.4" t="1.983"/>\r
+<eng-data cg="435." f="3356.08" m="1914.37" t="2.191"/>\r
+<eng-data cg="435." f="3270.48" m="1623.91" t="2.399"/>\r
+<eng-data cg="435." f="3182.6" m="1341.05" t="2.607"/>\r
+<eng-data cg="435." f="3098.31" m="1065.74" t="2.815"/>\r
+<eng-data cg="435." f="3002.95" m="798.309" t="3.023"/>\r
+<eng-data cg="435." f="2888.73" m="540.062" t="3.231"/>\r
+<eng-data cg="435." f="2266.61" m="314.09" t="3.439"/>\r
+<eng-data cg="435." f="1498.26" m="149.066" t="3.647"/>\r
+<eng-data cg="435." f="780.04" m="49.202" t="3.855"/>\r
+<eng-data cg="435." f="233.545" m="4.77393" t="4.063"/>\r
+<eng-data cg="435." f="0." m="0." t="4.16"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Animal Motor Works" code="N2800WW" Type="reloadable" dia="98." len="1213."\r
+initWt="13800." propWt="7694.7" delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="2660.58" peakThrust="3655.16" throatDia="0." exitDia="0."\r
+Itot="14816.8" burn-time="5.57" massFrac="55.76" Isp="196.35" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>@File: N2800b.txt, @Pts-I: 5383, @Pts-O: 31, @Sm: 8, @CO: 5%\r
+@TI: 14810.26, @TIa: 14792.71, @TIe: 0.0%, @ThMax: 3650.74, @ThAvg: 2770.17, @Tb: 5.34\r
+Exported using ThrustCurveTool, www.ThrustGear.com, by John DeMar\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="7694.7" cg="606.5"/>\r
+<eng-data t="0." f="93.0947" m="7694.7" cg="606.5"/>\r
+<eng-data t="0.002" f="168.347" m="7694.56" cg="606.5"/>\r
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+<eng-data t="0.019" f="1271.17" m="7688.39" cg="606.5"/>\r
+<eng-data t="0.029" f="1776.34" m="7680.47" cg="606.5"/>\r
+<eng-data t="0.043" f="2298.6" m="7665.66" cg="606.5"/>\r
+<eng-data t="0.062" f="2841.03" m="7640.3" cg="606.5"/>\r
+<eng-data t="0.072" f="3021.31" m="7625.08" cg="606.5"/>\r
+<eng-data t="0.084" f="3128.89" m="7605.92" cg="606.5"/>\r
+<eng-data t="0.14" f="3296.17" m="7512.49" cg="606.5"/>\r
+<eng-data t="0.277" f="3483.35" m="7271.32" cg="606.5"/>\r
+<eng-data t="0.293" f="3431.67" m="7242.59" cg="606.5"/>\r
+<eng-data t="0.369" f="3495.76" m="7105.88" cg="606.5"/>\r
+<eng-data t="0.978" f="3598.65" m="5984.01" cg="606.5"/>\r
+<eng-data t="1.973" f="3655.16" m="4109.89" cg="606.5"/>\r
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+<eng-data t="3.836" f="2223.91" m="801.635" cg="606.5"/>\r
+<eng-data t="4.109" f="1644.08" m="527.442" cg="606.5"/>\r
+<eng-data t="4.245" f="1443.68" m="418.401" cg="606.5"/>\r
+<eng-data t="4.272" f="1447.01" m="398.135" cg="606.5"/>\r
+<eng-data t="4.397" f="1163.58" m="313.401" cg="606.5"/>\r
+<eng-data t="4.489" f="1022.95" m="261.167" cg="606.5"/>\r
+<eng-data t="4.516" f="1057.2" m="246.583" cg="606.5"/>\r
+<eng-data t="4.574" f="883.885" m="217.35" cg="606.5"/>\r
+<eng-data t="4.647" f="776.407" m="185.878" cg="606.5"/>\r
+<eng-data t="5.569" f="0." m="0." cg="606.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Animal Motor Works 98-17500\r
-N4000BB 98 1213 0 6.1026 13.6683 AMW\r
-0.029 4207.591\r
-0.071 4709.549\r
-0.113 4906.310\r
-0.155 5007.780\r
-0.239 5041.557\r
-0.323 4993.595\r
-0.534 5046.912\r
-0.744 5145.819\r
-0.954 5248.063\r
-1.165 5293.196\r
-1.375 5232.456\r
-1.585 5209.528\r
-1.796 5165.473\r
-2.006 5047.698\r
-2.216 4913.086\r
-2.427 4783.447\r
-2.637 4659.163\r
-2.847 4195.994\r
-3.058 2850.731\r
-3.268 1981.973\r
-3.478 1295.536\r
-3.689 907.699\r
-3.899 490.196\r
-4.110 316.338\r
-4.207 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="272.02" Itot="16279.1" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="3866.78" burn-time="4.21" cgDiv="10" cgFix="1" cgStep="-1." code="N4000BB" delays="1000" dia="98." exitDia="0." initWt="13668.3" len="1213." mDiv="10" mFix="1" mStep="-1." massFrac="44.65" mfg="Animal Motor Works" peakThrust="5293.2" propWt="6102.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="606.5" f="0." m="6102.6" t="0."/>\r
+<eng-data cg="606.5" f="4207.59" m="6078.94" t="0.03"/>\r
+<eng-data cg="606.5" f="4709.55" m="6012.08" t="0.07"/>\r
+<eng-data cg="606.5" f="4906.31" m="5939.99" t="0.11"/>\r
+<eng-data cg="606.5" f="5007.78" m="5847.08" t="0.16"/>\r
+<eng-data cg="606.5" f="5041.56" m="5696.39" t="0.24"/>\r
+<eng-data cg="606.5" f="4993.6" m="5545.91" t="0.32"/>\r
+<eng-data cg="606.5" f="5046.91" m="5150.7" t="0.53"/>\r
+<eng-data cg="606.5" f="5145.82" m="4749.5" t="0.74"/>\r
+<eng-data cg="606.5" f="5248.06" m="4340.38" t="0.95"/>\r
+<eng-data cg="606.5" f="5293.2" m="3905.7" t="1.17"/>\r
+<eng-data cg="606.5" f="5232.46" m="3491.39" t="1.38"/>\r
+<eng-data cg="606.5" f="5209.53" m="3080.38" t="1.59"/>\r
+<eng-data cg="606.5" f="5165.47" m="2672." t="1.8"/>\r
+<eng-data cg="606.5" f="5047.7" m="2270." t="2.01"/>\r
+<eng-data cg="606.5" f="4913.09" m="1877.92" t="2.22"/>\r
+<eng-data cg="606.5" f="4783.45" m="1496.25" t="2.43"/>\r
+<eng-data cg="606.5" f="4659.16" m="1124.58" t="2.64"/>\r
+<eng-data cg="606.5" f="4195.99" m="776.024" t="2.85"/>\r
+<eng-data cg="606.5" f="2850.73" m="498.654" t="3.06"/>\r
+<eng-data cg="606.5" f="1981.97" m="308.431" t="3.27"/>\r
+<eng-data cg="606.5" f="1295.54" m="179.423" t="3.48"/>\r
+<eng-data cg="606.5" f="907.7" m="92.6996" t="3.69"/>\r
+<eng-data cg="606.5" f="490.2" m="37.6761" t="3.9"/>\r
+<eng-data cg="606.5" f="316.34" m="5.92936" t="4.11"/>\r
+<eng-data cg="606.5" f="0." m="0." t="4.21"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+D10 18 70 7 0.009800000000000001 0.0259 AT\r
+ 0.0070 23.0\r
+ 0.018 25.0\r
+ 0.027 20.25\r
+ 0.066 20.25\r
+ 0.073 18.5\r
+ 0.094 20.25\r
+ 0.112 20.75\r
+ 0.137 19.75\r
+ 0.163 21.5\r
+ 0.202 20.75\r
+ 0.231 20.75\r
+ 0.254 22.75\r
+ 0.27 20.75\r
+ 0.504 20.0\r
+ 0.536 18.25\r
+ 0.607 17.0\r
+ 0.687 14.75\r
+ 0.751 14.25\r
+ 0.84 11.25\r
+ 0.998 8.25\r
+ 1.024 8.25\r
+ 1.248 2.5\r
+ 1.385 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="199.6" Itot="19.183" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="11.284" burn-time="1.7" cgDiv="10" cgFix="1" cgStep="-1." code="D13" delays="4,7,10" dia="18." exitDia="0." initWt="33." len="70." mDiv="10" mFix="1" mStep="-1." massFrac="29.7" mfg="Aerotech" peakThrust="22.25" propWt="9.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <data>\r
+ <eng-data cg="35." f="0." m="9.8" t="0."/>\r
+ <eng-data cg="35." f="22.25" m="9.74317" t="0.01"/>\r
+ <eng-data cg="35." f="22.25" m="7.58344" t="0.2"/>\r
+ <eng-data cg="35." f="20." m="5.42499" t="0.4"/>\r
+ <eng-data cg="35." f="12.5" m="2.1043" t="0.8"/>\r
+ <eng-data cg="35." f="8." m="1.057" t="1."/>\r
+ <eng-data cg="35." f="1.34" m="0.102686" t="1.4"/>\r
+ <eng-data cg="35." f="0." m="0." t="1.7"/>\r
+ </data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="224.77" Itot="19.617" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="14.012" burn-time="1.4" cgDiv="10" cgFix="1" cgStep="-1." code="D15" delays="4,6" dia="24." exitDia="0." initWt="44." len="70." mDiv="10" mFix="1" mStep="-1." massFrac="20.23" mfg="Aerotech" peakThrust="28.5" propWt="8.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+ <eng-data cg="35." f="0." m="8.9" t="0."/>\r
+ <eng-data cg="35." f="26." m="8.84102" t="0.01"/>\r
+ <eng-data cg="35." f="28.5" m="7.72838" t="0.1"/>\r
+ <eng-data cg="35." f="23." m="4.22373" t="0.4"/>\r
+ <eng-data cg="35." f="11.2" m="1.12058" t="0.8"/>\r
+ <eng-data cg="35." f="4.5" m="0.408309" t="1."/>\r
+ <eng-data cg="35." f="0." m="0." t="1.4"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="208.09" Itot="19.59" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="20.841" burn-time="0.94" cgDiv="10" cgFix="1" cgStep="-1." code="D21" delays="4,7" dia="18." exitDia="0." initWt="25." len="70." mDiv="10" mFix="1" mStep="-1." massFrac="38.4" mfg="Aerotech" peakThrust="32.12" propWt="9.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech D21 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="9.6" t="0."/>\r
+<eng-data cg="35." f="1.367" m="9.59665" t="0.01"/>\r
+<eng-data cg="35." f="19.367" m="9.54077" t="0.021"/>\r
+<eng-data cg="35." f="32.12" m="9.43985" t="0.029"/>\r
+<eng-data cg="35." f="31.667" m="9.31481" t="0.037"/>\r
+<eng-data cg="35." f="30.528" m="9.10147" t="0.051"/>\r
+<eng-data cg="35." f="30.074" m="8.46298" t="0.094"/>\r
+<eng-data cg="35." f="31.213" m="8.14763" t="0.115"/>\r
+<eng-data cg="35." f="30.074" m="7.87734" t="0.133"/>\r
+<eng-data cg="35." f="30.76" m="7.2215" t="0.177"/>\r
+<eng-data cg="35." f="29.842" m="7.04331" t="0.189"/>\r
+<eng-data cg="35." f="30.528" m="6.83623" t="0.203"/>\r
+<eng-data cg="35." f="29.842" m="6.49602" t="0.226"/>\r
+<eng-data cg="35." f="28.935" m="5.79035" t="0.275"/>\r
+<eng-data cg="35." f="29.389" m="5.49025" t="0.296"/>\r
+<eng-data cg="35." f="28.027" m="4.99787" t="0.331"/>\r
+<eng-data cg="35." f="25.971" m="3.80712" t="0.421"/>\r
+<eng-data cg="35." f="24.146" m="3.10718" t="0.478"/>\r
+<eng-data cg="35." f="20.728" m="1.99669" t="0.579"/>\r
+<eng-data cg="35." f="17.774" m="1.242" t="0.659"/>\r
+<eng-data cg="35." f="14.356" m="0.612201" t="0.739"/>\r
+<eng-data cg="35." f="9.569" m="0.260477" t="0.799"/>\r
+<eng-data cg="35." f="4.557" m="0.0770365" t="0.852"/>\r
+<eng-data cg="35." f="1.139" m="0.0114421" t="0.899"/>\r
+<eng-data cg="35." f="0." m="0." t="0.94"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="208.18" Itot="19.599" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="21.776" burn-time="0.9" cgDiv="10" cgFix="1" cgStep="-1." code="D24" delays="4,7" dia="18." exitDia="0." initWt="31." len="70." mDiv="10" mFix="1" mStep="-1." massFrac="30.97" mfg="Aerotech" peakThrust="41.28" propWt="9.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="35." f="0." m="9.6" t="0."/>\r
+<eng-data cg="35." f="41.28" m="9.4989" t="0.01"/>\r
+<eng-data cg="35." f="36.38" m="7.78709" t="0.1"/>\r
+<eng-data cg="35." f="30.15" m="6.15766" t="0.2"/>\r
+<eng-data cg="35." f="25.26" m="3.44351" t="0.4"/>\r
+<eng-data cg="35." f="19.92" m="1.23046" t="0.6"/>\r
+<eng-data cg="35." f="16.8" m="0.331126" t="0.7"/>\r
+<eng-data cg="35." f="2.56" m="0.0940475" t="0.75"/>\r
+<eng-data cg="35." f="0." m="0." t="0.9"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="179.93" Itot="18.527" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="6.456" burn-time="2.87" cgDiv="10" cgFix="1" cgStep="-1." code="D7RC" delays="1000" dia="24." exitDia="0." initWt="42.2" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="24.88" mfg="Aerotech " peakThrust="10.99" propWt="10.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech D7 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="10.5" t="0."/>\r
+<eng-data cg="35." f="3.336" m="10.466" t="0.036"/>\r
+<eng-data cg="35." f="9.326" m="10.2937" t="0.084"/>\r
+<eng-data cg="35." f="10.281" m="10.1993" t="0.101"/>\r
+<eng-data cg="35." f="10.827" m="9.94808" t="0.143"/>\r
+<eng-data cg="35." f="10.99" m="9.51533" t="0.213"/>\r
+<eng-data cg="35." f="10.887" m="9.15578" t="0.271"/>\r
+<eng-data cg="35." f="10.685" m="8.61786" t="0.359"/>\r
+<eng-data cg="35." f="10.13" m="7.95726" t="0.471"/>\r
+<eng-data cg="35." f="10.342" m="7.75423" t="0.506"/>\r
+<eng-data cg="35." f="9.929" m="7.58765" t="0.535"/>\r
+<eng-data cg="35." f="8.697" m="6.13621" t="0.81"/>\r
+<eng-data cg="35." f="6.713" m="4.31969" t="1.226"/>\r
+<eng-data cg="35." f="5.138" m="3.10068" t="1.589"/>\r
+<eng-data cg="35." f="4.861" m="2.50285" t="1.8"/>\r
+<eng-data cg="35." f="4.581" m="1.56374" t="2.151"/>\r
+<eng-data cg="35." f="4.57" m="0.272392" t="2.649"/>\r
+<eng-data cg="35." f="3.887" m="0.15976" t="2.696"/>\r
+<eng-data cg="35." f="2.388" m="0.0672987" t="2.748"/>\r
+<eng-data cg="35." f="0.889" m="0.0125122" t="2.807"/>\r
+<eng-data cg="35." f="0.207" m="0.00164238" t="2.842"/>\r
+<eng-data cg="35." f="0." m="0." t="2.87"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="189.41" Itot="18.76" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="9.979" burn-time="1.88" cgDiv="10" cgFix="1" cgStep="-1." code="D9" delays="4,7" dia="24." exitDia="0." initWt="47.1" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="21.44" mfg="Aerotech" peakThrust="20." propWt="10.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <comments>Aerotech D9 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+ <data>\r
+ <eng-data cg="35." f="0." m="10.1" t="0."/>\r
+ <eng-data cg="35." f="2.204" m="10.0864" t="0.023"/>\r
+ <eng-data cg="35." f="1.653" m="10.0303" t="0.077"/>\r
+ <eng-data cg="35." f="4.96" m="9.85228" t="0.177"/>\r
+ <eng-data cg="35." f="8.817" m="9.51109" t="0.269"/>\r
+ <eng-data cg="35." f="9.92" m="9.31438" t="0.308"/>\r
+ <eng-data cg="35." f="9.368" m="9.27804" t="0.315"/>\r
+ <eng-data cg="35." f="10.604" m="9.04686" t="0.358"/>\r
+ <eng-data cg="35." f="11.94" m="8.70096" t="0.415"/>\r
+ <eng-data cg="35." f="13.917" m="8.00492" t="0.515"/>\r
+ <eng-data cg="35." f="16.675" m="7.11555" t="0.623"/>\r
+ <eng-data cg="35." f="19.155" m="6.0739" t="0.731"/>\r
+ <eng-data cg="35." f="20." m="5.43096" t="0.792"/>\r
+ <eng-data cg="35." f="19.155" m="4.66154" t="0.865"/>\r
+ <eng-data cg="35." f="19.562" m="4.41141" t="0.889"/>\r
+ <eng-data cg="35." f="18.6" m="4.06214" t="0.923"/>\r
+ <eng-data cg="35." f="16.12" m="2.98733" t="1.038"/>\r
+ <eng-data cg="35." f="14.195" m="2.35899" t="1.115"/>\r
+ <eng-data cg="35." f="12.538" m="1.85526" t="1.185"/>\r
+ <eng-data cg="35." f="10.336" m="1.28878" t="1.277"/>\r
+ <eng-data cg="35." f="7.44" m="0.829414" t="1.373"/>\r
+ <eng-data cg="35." f="4.822" m="0.459729" t="1.485"/>\r
+ <eng-data cg="35." f="2.755" m="0.200697" t="1.612"/>\r
+ <eng-data cg="35." f="1.24" m="0.0393873" t="1.762"/>\r
+ <eng-data cg="35." f="0." m="0." t="1.88"/>\r
+ </data>\r
+ </engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Based On NAR Test Data\r
-;12/23/93\r
-E11J 24 70 4 0.025 0.0624 Aerotech\r
-0.0725446 14.3704\r
-0.16183 17.6296\r
-0.206473 18.3704\r
-0.418527 19.2593\r
-0.731027 18.3704\r
-1.31696 14.2222\r
-1.91964 9.03704\r
-2.51116 2.22222\r
-2.83 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="134.05" Itot="32.865" Type="unspecified" auto-calc-cg="1" auto-calc-mass="1" avgThrust="11.613" burn-time="2.83" cgDiv="10" cgFix="1" cgStep="-1." code="E11J" delays="4" dia="24." exitDia="0." initWt="62.4" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="40.06" mfg="Aerotech" peakThrust="19.259" propWt="25." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Based On NAR Test Data\r
+12/23/93\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="25." t="0."/>\r
+<eng-data cg="35." f="14.3704" m="24.6035" t="0.0725446"/>\r
+<eng-data cg="35." f="17.6296" m="23.5168" t="0.16183"/>\r
+<eng-data cg="35." f="18.3704" m="22.9055" t="0.206473"/>\r
+<eng-data cg="35." f="19.2593" m="19.8705" t="0.418527"/>\r
+<eng-data cg="35." f="18.3704" m="15.3979" t="0.731027"/>\r
+<eng-data cg="35." f="14.2222" m="8.13432" t="1.31696"/>\r
+<eng-data cg="35." f="9.03704" m="2.80264" t="1.91964"/>\r
+<eng-data cg="35." f="2.22222" m="0.269489" t="2.51116"/>\r
+<eng-data cg="35." f="0." m="0." t="2.83"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-;Aerotech E12JRC RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-E12JRC 24 70 100 0.0303 0.0594 AT\r
-0.054 16.764\r
-0.095 18.33\r
-0.197 16.545\r
-0.313 16.654\r
-0.36 17.211\r
-0.401 16.316\r
-0.442 17.55\r
-0.476 16.206\r
-0.578 16.316\r
-0.666 16.764\r
-0.7 15.649\r
-0.768 16.316\r
-0.89 16.097\r
-1.019 15.649\r
-1.162 14.983\r
-1.23 14.983\r
-1.25 13.968\r
-1.291 14.754\r
-1.332 13.749\r
-1.373 14.197\r
-1.434 13.53\r
-1.488 13.749\r
-1.597 12.635\r
-1.726 11.401\r
-1.828 10.615\r
-1.889 9.613\r
-1.957 9.613\r
-1.998 8.495\r
-2.093 8.607\r
-2.277 7.042\r
-2.487 5.813\r
-3.05 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="115.17" Itot="34.222" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="11.22" burn-time="3.05" cgDiv="10" cgFix="1" cgStep="-1." code="E12JRC" delays="1000" dia="24." exitDia="0." initWt="59.4" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="51.01" mfg="Aerotech" peakThrust="18.33" propWt="30.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech E12JRC RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="30.3" t="0."/>\r
+<eng-data cg="35." f="16.764" m="29.8992" t="0.054"/>\r
+<eng-data cg="35." f="18.33" m="29.2623" t="0.095"/>\r
+<eng-data cg="35." f="16.545" m="27.6875" t="0.197"/>\r
+<eng-data cg="35." f="16.654" m="25.9826" t="0.313"/>\r
+<eng-data cg="35." f="17.211" m="25.278" t="0.36"/>\r
+<eng-data cg="35." f="16.316" m="24.6695" t="0.401"/>\r
+<eng-data cg="35." f="17.55" m="24.0548" t="0.442"/>\r
+<eng-data cg="35." f="16.206" m="23.5467" t="0.476"/>\r
+<eng-data cg="35." f="16.316" m="22.0782" t="0.578"/>\r
+<eng-data cg="35." f="16.764" m="20.7895" t="0.666"/>\r
+<eng-data cg="35." f="15.649" m="20.3016" t="0.7"/>\r
+<eng-data cg="35." f="16.316" m="19.3393" t="0.768"/>\r
+<eng-data cg="35." f="16.097" m="17.5887" t="0.89"/>\r
+<eng-data cg="35." f="15.649" m="15.7758" t="1.019"/>\r
+<eng-data cg="35." f="14.983" m="13.8366" t="1.162"/>\r
+<eng-data cg="35." f="14.983" m="12.9346" t="1.23"/>\r
+<eng-data cg="35." f="13.968" m="12.6782" t="1.25"/>\r
+<eng-data cg="35." f="14.754" m="12.1569" t="1.291"/>\r
+<eng-data cg="35." f="13.749" m="11.6396" t="1.332"/>\r
+<eng-data cg="35." f="14.197" m="11.1323" t="1.373"/>\r
+<eng-data cg="35." f="13.53" m="10.3836" t="1.434"/>\r
+<eng-data cg="35." f="13.749" m="9.73145" t="1.488"/>\r
+<eng-data cg="35." f="12.635" m="8.45831" t="1.597"/>\r
+<eng-data cg="35." f="11.401" m="7.08567" t="1.726"/>\r
+<eng-data cg="35." f="10.615" m="6.09154" t="1.828"/>\r
+<eng-data cg="35." f="9.613" m="5.54529" t="1.889"/>\r
+<eng-data cg="35." f="9.613" m="4.96652" t="1.957"/>\r
+<eng-data cg="35." f="8.495" m="4.63785" t="1.998"/>\r
+<eng-data cg="35." f="8.607" m="3.91861" t="2.093"/>\r
+<eng-data cg="35." f="7.042" m="2.6439" t="2.277"/>\r
+<eng-data cg="35." f="5.813" m="1.44882" t="2.487"/>\r
+<eng-data cg="35." f="0." m="0." t="3.05"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="201.71" Itot="39.759" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="15.06" burn-time="2.64" cgDiv="10" cgFix="1" cgStep="-1." code="E15" delays="4,7" dia="24." exitDia="0." initWt="50.1" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="40.12" mfg="Aerotech" peakThrust="28.84" propWt="20.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech E15 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="20.1" t="0."/>\r
+<eng-data cg="35." f="23.33" m="19.9821" t="0.02"/>\r
+<eng-data cg="35." f="27.318" m="19.7772" t="0.036"/>\r
+<eng-data cg="35." f="28.84" m="19.4649" t="0.058"/>\r
+<eng-data cg="35." f="27.171" m="19.1676" t="0.079"/>\r
+<eng-data cg="35." f="25.638" m="18.3667" t="0.139"/>\r
+<eng-data cg="35." f="24.263" m="17.8117" t="0.183"/>\r
+<eng-data cg="35." f="24.106" m="17.1515" t="0.237"/>\r
+<eng-data cg="35." f="22.426" m="16.4457" t="0.297"/>\r
+<eng-data cg="35." f="21.964" m="15.593" t="0.373"/>\r
+<eng-data cg="35." f="20.894" m="15.3005" t="0.4"/>\r
+<eng-data cg="35." f="21.355" m="14.8413" t="0.443"/>\r
+<eng-data cg="35." f="20.442" m="14.3764" t="0.487"/>\r
+<eng-data cg="35." f="19.833" m="13.0529" t="0.617"/>\r
+<eng-data cg="35." f="18.457" m="11.8431" t="0.742"/>\r
+<eng-data cg="35." f="20." m="11.1626" t="0.812"/>\r
+<eng-data cg="35." f="18.006" m="10.7976" t="0.85"/>\r
+<eng-data cg="35." f="18.467" m="10.3458" t="0.899"/>\r
+<eng-data cg="35." f="17.711" m="9.10213" t="1.035"/>\r
+<eng-data cg="35." f="16.945" m="8.53273" t="1.1"/>\r
+<eng-data cg="35." f="16.945" m="8.01874" t="1.16"/>\r
+<eng-data cg="35." f="15.736" m="6.22613" t="1.377"/>\r
+<eng-data cg="35." f="14.656" m="5.8497" t="1.426"/>\r
+<eng-data cg="35." f="16.198" m="5.77171" t="1.436"/>\r
+<eng-data cg="35." f="14.813" m="5.56006" t="1.463"/>\r
+<eng-data cg="35." f="14.361" m="4.91849" t="1.55"/>\r
+<eng-data cg="35." f="15.432" m="4.75281" t="1.572"/>\r
+<eng-data cg="35." f="13.752" m="4.47248" t="1.61"/>\r
+<eng-data cg="35." f="12.839" m="3.01392" t="1.827"/>\r
+<eng-data cg="35." f="10.098" m="1.28036" t="2.126"/>\r
+<eng-data cg="35." f="6.116" m="0.41559" t="2.337"/>\r
+<eng-data cg="35." f="1.369" m="0.0352967" t="2.538"/>\r
+<eng-data cg="35." f="0." m="0." t="2.64"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Aerotech E15 RASP.ENG file made from NAR published data\r
-; File produced July 4, 2000\r
-; Submitted to ThrustCurve.org by Chris Kobel (3/30/07)\r
-; The total impulse, peak thrust, average thrust and burn time are\r
-; the same as the averaged static test data on the NAR web site in\r
-; the certification file. The curve drawn with these data points is as\r
-; close to the certification curve as can be with such a limited\r
-; number of points (32) allowed with wRASP up to v1.6.\r
-E15W 24 70 4-7 .0201 .0501 AT\r
- 0.020 23.330\r
- 0.036 27.318\r
- 0.058 28.840\r
- 0.079 27.171\r
- 0.139 25.638\r
- 0.183 24.263\r
- 0.237 24.106\r
- 0.297 22.426\r
- 0.373 21.964\r
- 0.400 20.894\r
- 0.443 21.355\r
- 0.487 20.442\r
- 0.617 19.833\r
- 0.742 18.457\r
- 0.812 20.000\r
- 0.850 18.006\r
- 0.899 18.467\r
- 1.035 17.711\r
- 1.100 16.945\r
- 1.160 16.945\r
- 1.377 15.736\r
- 1.426 14.656\r
- 1.436 16.198\r
- 1.463 14.813\r
- 1.550 14.361\r
- 1.572 15.432\r
- 1.610 13.752\r
- 1.827 12.839\r
- 2.126 10.098\r
- 2.337 6.116\r
- 2.538 1.369\r
- 2.600 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="205.82" Itot="38.35" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="14.099" burn-time="2.72" cgDiv="10" cgFix="1" cgStep="-1." code="E16" delays="4,7" dia="29." exitDia="0." initWt="107." len="121." mDiv="10" mFix="1" mStep="-1." massFrac="17.76" mfg="Aerotech" peakThrust="27.92" propWt="19." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="60.5" f="0." m="19." t="0."/>\r
+<eng-data cg="60.5" f="27.92" m="18.7233" t="0.04"/>\r
+<eng-data cg="60.5" f="23.5" m="17.1948" t="0.16"/>\r
+<eng-data cg="60.5" f="21.4" m="16.0826" t="0.26"/>\r
+<eng-data cg="60.5" f="10.9" m="2.16039" t="2."/>\r
+<eng-data cg="60.5" f="6.36" m="0.535663" t="2.38"/>\r
+<eng-data cg="60.5" f="0." m="0." t="2.72"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="195.96" Itot="39.78" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="18.082" burn-time="2.2" cgDiv="10" cgFix="1" cgStep="-1." code="E18" delays="4,8" dia="24." exitDia="0." initWt="57." len="70." mDiv="10" mFix="1" mStep="-1." massFrac="36.32" mfg="Aerotech" peakThrust="31." propWt="20.7" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="35." f="0." m="20.7" t="0."/>\r
+<eng-data cg="35." f="31." m="20.3774" t="0.04"/>\r
+<eng-data cg="35." f="30." m="14.6638" t="0.4"/>\r
+<eng-data cg="35." f="26.7" m="8.7629" t="0.8"/>\r
+<eng-data cg="35." f="19.1" m="3.99638" t="1.2"/>\r
+<eng-data cg="35." f="8." m="1.17602" t="1.6"/>\r
+<eng-data cg="35." f="2.2" m="0.11448" t="2."/>\r
+<eng-data cg="35." f="0." m="0." t="2.2"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+; @File: E20.txt, @Pts-I: 1001, @Pts-O: 32, @Sm: 3, @CO: 5%\r
+; @TI: 34.6666, @TIa: 34.5451, @TIe: 0.0%, @ThMax: 34.6991, @ThAvg: 22.1301, @Tb: 1.561\r
+; Exported using ThrustCurveTool, www.ThrustGear.com\r
+E22 24 65 4-7-10 0.0162 0.049 A\r
+0.0 0.0290422\r
+0.024 0.227567\r
+0.038 1.394029\r
+0.048 2.6721\r
+0.056 5.81661\r
+0.06 7.76916\r
+0.062 9.00446\r
+0.064 10.71764\r
+0.072 20.3365\r
+0.074 22.4147\r
+0.08 27.1311\r
+0.084 28.9874\r
+0.09 30.5394\r
+0.104 32.9513\r
+0.124 34.2647\r
+0.138 34.677\r
+0.252 33.8465\r
+0.36 32.0816\r
+0.63 29.8124\r
+0.672 28.8301\r
+0.77 27.3596\r
+0.8 26.3903\r
+0.9 24.2069\r
+1.084 18.06808\r
+1.134 16.89181\r
+1.16 15.87009\r
+1.2899 12.19213\r
+1.3719 9.38065\r
+1.5079 4.03928\r
+1.5519 2.72185\r
+1.6019 1.720821\r
+1.7579 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="207.01" Itot="35.323" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="22.498" burn-time="1.57" cgDiv="10" cgFix="1" cgStep="-1." code="E23" delays="5,8" dia="29." exitDia="0." initWt="103.9" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="16.75" mfg="Aerotech" peakThrust="38.22" propWt="17.4" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech E23 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="62." f="0." m="17.4" t="0."/>\r
+<eng-data cg="62." f="16.299" m="17.3037" t="0.024"/>\r
+<eng-data cg="62." f="21.959" m="17.2" t="0.035"/>\r
+<eng-data cg="62." f="30.785" m="16.7843" t="0.067"/>\r
+<eng-data cg="62." f="35.774" m="16.4072" t="0.09"/>\r
+<eng-data cg="62." f="37.577" m="15.2691" t="0.153"/>\r
+<eng-data cg="62." f="38.22" m="14.3916" t="0.2"/>\r
+<eng-data cg="62." f="37.357" m="13.647" t="0.24"/>\r
+<eng-data cg="62." f="37.577" m="12.1336" t="0.322"/>\r
+<eng-data cg="62." f="35.093" m="10.8628" t="0.393"/>\r
+<eng-data cg="62." f="32.378" m="8.51964" t="0.534"/>\r
+<eng-data cg="62." f="27.168" m="5.68905" t="0.727"/>\r
+<eng-data cg="62." f="26.938" m="5.16932" t="0.766"/>\r
+<eng-data cg="62." f="25.125" m="4.75898" t="0.798"/>\r
+<eng-data cg="62." f="21.729" m="3.48956" t="0.908"/>\r
+<eng-data cg="62." f="16.98" m="2.06898" t="1.057"/>\r
+<eng-data cg="62." f="12.682" m="1.11923" t="1.187"/>\r
+<eng-data cg="62." f="7.471" m="0.379638" t="1.336"/>\r
+<eng-data cg="62." f="3.169" m="0.0808848" t="1.45"/>\r
+<eng-data cg="62." f="1.584" m="0.0258633" t="1.497"/>\r
+<eng-data cg="62." f="0.679" m="0.00635506" t="1.532"/>\r
+<eng-data cg="62." f="0." m="0." t="1.57"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="219.95" Itot="39.689" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="32.532" burn-time="1.22" cgDiv="10" cgFix="1" cgStep="-1." code="E28" delays="2,5,8" dia="24." exitDia="0." initWt="54.5" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="33.76" mfg="Aerotech" peakThrust="50.52" propWt="18.4" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech E28 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="18.4" t="0."/>\r
+<eng-data cg="35." f="29.862" m="18.3308" t="0.01"/>\r
+<eng-data cg="35." f="45.139" m="18.1917" t="0.018"/>\r
+<eng-data cg="35." f="47.562" m="17.7619" t="0.038"/>\r
+<eng-data cg="35." f="50.52" m="16.7843" t="0.081"/>\r
+<eng-data cg="35." f="48.953" m="16.2078" t="0.106"/>\r
+<eng-data cg="35." f="48.263" m="15.3064" t="0.146"/>\r
+<eng-data cg="35." f="48.953" m="14.9684" t="0.161"/>\r
+<eng-data cg="35." f="48.953" m="14.1514" t="0.197"/>\r
+<eng-data cg="35." f="47.562" m="13.1447" t="0.242"/>\r
+<eng-data cg="35." f="46.18" m="11.6018" t="0.313"/>\r
+<eng-data cg="35." f="43.057" m="9.57468" t="0.411"/>\r
+<eng-data cg="35." f="40.624" m="7.96469" t="0.494"/>\r
+<eng-data cg="35." f="39.583" m="7.35115" t="0.527"/>\r
+<eng-data cg="35." f="40.274" m="7.07349" t="0.542"/>\r
+<eng-data cg="35." f="38.542" m="6.70809" t="0.562"/>\r
+<eng-data cg="35." f="36.46" m="5.47371" t="0.633"/>\r
+<eng-data cg="35." f="34.377" m="4.6527" t="0.683"/>\r
+<eng-data cg="35." f="31.244" m="3.74004" t="0.743"/>\r
+<eng-data cg="35." f="29.162" m="2.95591" t="0.799"/>\r
+<eng-data cg="35." f="26.038" m="1.95786" t="0.877"/>\r
+<eng-data cg="35." f="20.832" m="0.947455" t="0.97"/>\r
+<eng-data cg="35." f="17.359" m="0.628755" t="1.006"/>\r
+<eng-data cg="35." f="11.462" m="0.361524" t="1.046"/>\r
+<eng-data cg="35." f="6.943" m="0.178072" t="1.089"/>\r
+<eng-data cg="35." f="3.819" m="0.0708017" t="1.132"/>\r
+<eng-data cg="35." f="1.735" m="0.0193045" t="1.172"/>\r
+<eng-data cg="35." f="0." m="0." t="1.22"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="203.49" Itot="39.512" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="32.387" burn-time="1.22" cgDiv="10" cgFix="1" cgStep="-1." code="E30" delays="4,7" dia="24." exitDia="0." initWt="43.3" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="45.73" mfg="Aerotech" peakThrust="48.27" propWt="19.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech E30 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="19.8" t="0."/>\r
+<eng-data cg="35." f="38.847" m="19.6735" t="0.013"/>\r
+<eng-data cg="35." f="45.621" m="19.5253" t="0.02"/>\r
+<eng-data cg="35." f="48.27" m="19.0313" t="0.041"/>\r
+<eng-data cg="35." f="46.502" m="18.6039" t="0.059"/>\r
+<eng-data cg="35." f="46.502" m="17.4154" t="0.11"/>\r
+<eng-data cg="35." f="45.912" m="16.1187" t="0.166"/>\r
+<eng-data cg="35." f="46.792" m="15.7006" t="0.184"/>\r
+<eng-data cg="35." f="45.912" m="14.9341" t="0.217"/>\r
+<eng-data cg="35." f="45.912" m="13.8298" t="0.265"/>\r
+<eng-data cg="35." f="45.031" m="12.5993" t="0.319"/>\r
+<eng-data cg="35." f="44.15" m="11.1692" t="0.383"/>\r
+<eng-data cg="35." f="42.089" m="9.03006" t="0.482"/>\r
+<eng-data cg="35." f="38.847" m="6.7588" t="0.594"/>\r
+<eng-data cg="35." f="39.437" m="6.3469" t="0.615"/>\r
+<eng-data cg="35." f="37.376" m="6.0967" t="0.628"/>\r
+<eng-data cg="35." f="35.314" m="5.07677" t="0.684"/>\r
+<eng-data cg="35." f="33.263" m="4.08018" t="0.742"/>\r
+<eng-data cg="35." f="30.021" m="3.0971" t="0.804"/>\r
+<eng-data cg="35." f="25.607" m="2.03781" t="0.88"/>\r
+<eng-data cg="35." f="20.014" m="1.10049" t="0.962"/>\r
+<eng-data cg="35." f="12.949" m="0.472798" t="1.038"/>\r
+<eng-data cg="35." f="7.358" m="0.213307" t="1.089"/>\r
+<eng-data cg="35." f="3.237" m="0.0487181" t="1.151"/>\r
+<eng-data cg="35." f="1.176" m="0.0100183" t="1.186"/>\r
+<eng-data cg="35." f="0." m="0." t="1.22"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="177.84" Itot="37.496" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="5.266" burn-time="7.12" cgDiv="10" cgFix="1" cgStep="-1." code="E6-RC" delays="1000" dia="24." exitDia="0." initWt="52.7" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="40.8" mfg="Aerotech" peakThrust="11.9" propWt="21.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech E6TRC RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="21.5" t="0."/>\r
+<eng-data cg="35." f="10.866" m="21.3536" t="0.047"/>\r
+<eng-data cg="35." f="11.693" m="20.8362" t="0.127"/>\r
+<eng-data cg="35." f="11.9" m="20.41" t="0.19"/>\r
+<eng-data cg="35." f="11.622" m="19.5603" t="0.316"/>\r
+<eng-data cg="35." f="10.593" m="18.2483" t="0.522"/>\r
+<eng-data cg="35." f="9.287" m="16.9887" t="0.743"/>\r
+<eng-data cg="35." f="7.842" m="15.7463" t="0.996"/>\r
+<eng-data cg="35." f="6.19" m="14.7284" t="1.249"/>\r
+<eng-data cg="35." f="5.296" m="14.0007" t="1.47"/>\r
+<eng-data cg="35." f="4.747" m="13.0879" t="1.787"/>\r
+<eng-data cg="35." f="4.471" m="11.5419" t="2.372"/>\r
+<eng-data cg="35." f="4.403" m="9.8933" t="3.02"/>\r
+<eng-data cg="35." f="4.264" m="8.08683" t="3.747"/>\r
+<eng-data cg="35." f="4.403" m="6.24061" t="4.49"/>\r
+<eng-data cg="35." f="4.333" m="4.02404" t="5.375"/>\r
+<eng-data cg="35." f="4.264" m="2.26914" t="6.087"/>\r
+<eng-data cg="35." f="4.264" m="0.723924" t="6.719"/>\r
+<eng-data cg="35." f="4.196" m="0.3407" t="6.877"/>\r
+<eng-data cg="35." f="3.783" m="0.157694" t="6.957"/>\r
+<eng-data cg="35." f="2.614" m="0.0714955" t="7.004"/>\r
+<eng-data cg="35." f="1.513" m="0.0336329" t="7.036"/>\r
+<eng-data cg="35." f="0.55" m="0.00583432" t="7.083"/>\r
+<eng-data cg="35." f="0." m="0." t="7.12"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech E7TRC RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-E7RC 24 70 100 0.0171 0.0484 AT\r
-0.038 6.636\r
-0.063 10.056\r
-0.087 11.019\r
-0.134 11.42\r
-0.206 11.58\r
-0.312 11.149\r
-0.466 10.738\r
-0.667 9.777\r
-0.94 8.132\r
-1.223 6.281\r
-1.484 5.182\r
-1.709 4.701\r
-2.112 4.423\r
-2.776 4.279\r
-3.31 4.205\r
-3.926 4.266\r
-4.401 4.192\r
-4.638 4.258\r
-4.744 4.119\r
-5.124 3.979\r
-5.219 3.977\r
-5.266 3.156\r
-5.313 1.992\r
-5.36 0.965\r
-5.43 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="175.03" Itot="29.351" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="5.405" burn-time="5.43" cgDiv="10" cgFix="1" cgStep="-1." code="E7RC" delays="1000" dia="24." exitDia="0." initWt="48.4" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="35.33" mfg="Aerotech" peakThrust="11.58" propWt="17.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech E7TRC RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="17.1" t="0."/>\r
+<eng-data cg="35." f="6.636" m="17.0265" t="0.038"/>\r
+<eng-data cg="35." f="10.056" m="16.905" t="0.063"/>\r
+<eng-data cg="35." f="11.019" m="16.7576" t="0.087"/>\r
+<eng-data cg="35." f="11.42" m="16.4504" t="0.134"/>\r
+<eng-data cg="35." f="11.58" m="15.968" t="0.206"/>\r
+<eng-data cg="35." f="11.149" m="15.2662" t="0.312"/>\r
+<eng-data cg="35." f="10.738" m="14.2843" t="0.466"/>\r
+<eng-data cg="35." f="9.777" m="13.0831" t="0.667"/>\r
+<eng-data cg="35." f="8.132" m="11.6589" t="0.94"/>\r
+<eng-data cg="35." f="6.281" m="10.4707" t="1.223"/>\r
+<eng-data cg="35." f="5.182" m="9.59916" t="1.484"/>\r
+<eng-data cg="35." f="4.701" m="8.95139" t="1.709"/>\r
+<eng-data cg="35." f="4.423" m="7.88027" t="2.112"/>\r
+<eng-data cg="35." f="4.279" m="6.19708" t="2.776"/>\r
+<eng-data cg="35." f="4.205" m="4.87734" t="3.31"/>\r
+<eng-data cg="35." f="4.266" m="3.35727" t="3.926"/>\r
+<eng-data cg="35." f="4.192" m="2.18694" t="4.401"/>\r
+<eng-data cg="35." f="4.258" m="1.60356" t="4.638"/>\r
+<eng-data cg="35." f="4.119" m="1.34489" t="4.744"/>\r
+<eng-data cg="35." f="3.979" m="0.448479" t="5.124"/>\r
+<eng-data cg="35." f="3.977" m="0.228306" t="5.219"/>\r
+<eng-data cg="35." f="3.156" m="0.130646" t="5.266"/>\r
+<eng-data cg="35." f="1.992" m="0.0601628" t="5.313"/>\r
+<eng-data cg="35." f="0.965" m="0.0196776" t="5.36"/>\r
+<eng-data cg="35." f="0." m="0." t="5.43"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="145.37" Itot="43.195" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="14.742" burn-time="2.93" cgDiv="10" cgFix="1" cgStep="-1." code="F12" delays="2,5" dia="24." exitDia="0." initWt="66.7" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="45.43" mfg="Aerotech" peakThrust="23.54" propWt="30.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F12 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="30.3" t="0."/>\r
+<eng-data cg="35." f="20.894" m="30.0289" t="0.037"/>\r
+<eng-data cg="35." f="22.152" m="29.7722" t="0.054"/>\r
+<eng-data cg="35." f="22.152" m="29.0419" t="0.101"/>\r
+<eng-data cg="35." f="22.571" m="28.3046" t="0.148"/>\r
+<eng-data cg="35." f="23.409" m="28.0305" t="0.165"/>\r
+<eng-data cg="35." f="22.421" m="27.4679" t="0.2"/>\r
+<eng-data cg="35." f="22.142" m="26.2019" t="0.281"/>\r
+<eng-data cg="35." f="22.132" m="24.8354" t="0.369"/>\r
+<eng-data cg="35." f="22.271" m="23.2002" t="0.474"/>\r
+<eng-data cg="35." f="23.54" m="22.3647" t="0.526"/>\r
+<eng-data cg="35." f="21.982" m="21.9974" t="0.549"/>\r
+<eng-data cg="35." f="22.122" m="20.6362" t="0.637"/>\r
+<eng-data cg="35." f="21.842" m="19.2947" t="0.724"/>\r
+<eng-data cg="35." f="21.413" m="18.1417" t="0.8"/>\r
+<eng-data cg="35." f="22.251" m="17.7895" t="0.823"/>\r
+<eng-data cg="35." f="20.714" m="17.4429" t="0.846"/>\r
+<eng-data cg="35." f="21.553" m="16.924" t="0.881"/>\r
+<eng-data cg="35." f="21.123" m="15.9661" t="0.945"/>\r
+<eng-data cg="35." f="20.704" m="14.8511" t="1.021"/>\r
+<eng-data cg="35." f="20.554" m="13.5054" t="1.114"/>\r
+<eng-data cg="35." f="19.296" m="12.1217" t="1.213"/>\r
+<eng-data cg="35." f="18.298" m="9.89334" t="1.382"/>\r
+<eng-data cg="35." f="18.019" m="8.63232" t="1.481"/>\r
+<eng-data cg="35." f="15.343" m="5.63682" t="1.737"/>\r
+<eng-data cg="35." f="17.3" m="5.03003" t="1.79"/>\r
+<eng-data cg="35." f="13.936" m="4.01116" t="1.883"/>\r
+<eng-data cg="35." f="11.26" m="2.52654" t="2.051"/>\r
+<eng-data cg="35." f="7.468" m="1.41646" t="2.22"/>\r
+<eng-data cg="35." f="3.671" m="0.529609" t="2.447"/>\r
+<eng-data cg="35." f="1.135" m="0.0879761" t="2.709"/>\r
+<eng-data cg="35." f="0." m="0." t="2.93"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech F13RCJ RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-F13RCJ 32 107 100 0.0323 0.1105 AT\r
-0.048 15.309\r
-0.084 18.629\r
-0.143 19.98\r
-0.311 18.968\r
-0.538 18.172\r
-0.729 17.138\r
-0.992 15.428\r
-1.279 13.828\r
-1.673 12.456\r
-1.984 11.879\r
-2.044 12.227\r
-2.139 11.313\r
-2.378 11.193\r
-2.51 11.084\r
-2.558 12.108\r
-2.641 10.855\r
-2.976 10.736\r
-3.49 10.627\r
-3.873 10.507\r
-3.992 10.965\r
-4.028 10.627\r
-4.41 10.507\r
-4.625 10.736\r
-4.769 9.941\r
-4.829 8.684\r
-4.865 6.742\r
-4.96 3.199\r
-5.02 1.485\r
-5.1 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="195.95" Itot="62.067" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="12.17" burn-time="5.1" cgDiv="10" cgFix="1" cgStep="-1." code="F13RCJ" delays="1000" dia="32." exitDia="0." initWt="110.5" len="107." mDiv="10" mFix="1" mStep="-1." massFrac="29.23" mfg="Aerotech" peakThrust="19.98" propWt="32.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F13RCJ RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="53.5" f="0." m="32.3" t="0."/>\r
+<eng-data cg="53.5" f="15.309" m="32.1088" t="0.048"/>\r
+<eng-data cg="53.5" f="18.629" m="31.7909" t="0.084"/>\r
+<eng-data cg="53.5" f="19.98" m="31.1982" t="0.143"/>\r
+<eng-data cg="53.5" f="18.968" m="29.4956" t="0.311"/>\r
+<eng-data cg="53.5" f="18.172" m="27.3019" t="0.538"/>\r
+<eng-data cg="53.5" f="17.138" m="25.5471" t="0.729"/>\r
+<eng-data cg="53.5" f="15.428" m="23.3185" t="0.992"/>\r
+<eng-data cg="53.5" f="13.828" m="21.1337" t="1.279"/>\r
+<eng-data cg="53.5" f="12.456" m="18.4391" t="1.673"/>\r
+<eng-data cg="53.5" f="11.879" m="16.4698" t="1.984"/>\r
+<eng-data cg="53.5" f="12.227" m="16.0935" t="2.044"/>\r
+<eng-data cg="53.5" f="11.313" m="15.5116" t="2.139"/>\r
+<eng-data cg="53.5" f="11.193" m="14.112" t="2.378"/>\r
+<eng-data cg="53.5" f="11.084" m="13.3469" t="2.51"/>\r
+<eng-data cg="53.5" f="12.108" m="13.0572" t="2.558"/>\r
+<eng-data cg="53.5" f="10.855" m="12.5613" t="2.641"/>\r
+<eng-data cg="53.5" f="10.736" m="10.6793" t="2.976"/>\r
+<eng-data cg="53.5" f="10.627" m="7.82211" t="3.49"/>\r
+<eng-data cg="53.5" f="10.507" m="5.71596" t="3.873"/>\r
+<eng-data cg="53.5" f="10.965" m="5.0511" t="3.992"/>\r
+<eng-data cg="53.5" f="10.627" m="4.84884" t="4.028"/>\r
+<eng-data cg="53.5" f="10.507" m="2.74819" t="4.41"/>\r
+<eng-data cg="53.5" f="10.736" m="1.55979" t="4.625"/>\r
+<eng-data cg="53.5" f="9.941" m="0.785045" t="4.769"/>\r
+<eng-data cg="53.5" f="8.684" m="0.49427" t="4.829"/>\r
+<eng-data cg="53.5" f="6.742" m="0.349771" t="4.865"/>\r
+<eng-data cg="53.5" f="3.199" m="0.104039" t="4.96"/>\r
+<eng-data cg="53.5" f="1.485" m="0.0309119" t="5.02"/>\r
+<eng-data cg="53.5" f="0." m="0." t="5.1"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech F16RCJ RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-F16RCJ 32 107 100 0.0625 0.1404 AT\r
-0.046 26.35\r
-0.116 22.388\r
-0.139 21.374\r
-0.185 21.886\r
-0.22 20.54\r
-0.301 19.696\r
-0.498 18.35\r
-0.579 19.194\r
-0.637 16.492\r
-0.718 18.35\r
-0.834 18.35\r
-0.95 18.35\r
-1.054 19.194\r
-1.147 17.848\r
-1.181 18.853\r
-1.263 17.336\r
-1.436 18.009\r
-1.633 17.165\r
-1.784 17.336\r
-1.865 18.682\r
-1.934 16.834\r
-1.981 17.336\r
-2.178 16.332\r
-2.375 16.332\r
-2.502 18.18\r
-2.664 15.659\r
-2.896 15.488\r
-3.29 13.8\r
-3.718 11.611\r
-4.181 9.426\r
-4.888 5.891\r
-5.69 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="123.15" Itot="75.483" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="13.266" burn-time="5.69" cgDiv="10" cgFix="1" cgStep="-1." code="F16RCJ" delays="1000" dia="32." exitDia="0." initWt="140.4" len="107." mDiv="10" mFix="1" mStep="-1." massFrac="44.52" mfg="Aerotech" peakThrust="26.35" propWt="62.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F16RCJ RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="53.5" f="0." m="62.5" t="0."/>\r
+<eng-data cg="53.5" f="26.35" m="61.9982" t="0.046"/>\r
+<eng-data cg="53.5" f="22.388" m="60.5858" t="0.116"/>\r
+<eng-data cg="53.5" f="21.374" m="60.1691" t="0.139"/>\r
+<eng-data cg="53.5" f="21.886" m="59.3452" t="0.185"/>\r
+<eng-data cg="53.5" f="20.54" m="58.7305" t="0.22"/>\r
+<eng-data cg="53.5" f="19.696" m="57.3812" t="0.301"/>\r
+<eng-data cg="53.5" f="18.35" m="54.2783" t="0.498"/>\r
+<eng-data cg="53.5" f="19.194" m="53.0193" t="0.579"/>\r
+<eng-data cg="53.5" f="16.492" m="52.1624" t="0.637"/>\r
+<eng-data cg="53.5" f="18.35" m="50.994" t="0.718"/>\r
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+<eng-data cg="53.5" f="17.848" m="44.4264" t="1.147"/>\r
+<eng-data cg="53.5" f="18.853" m="43.9098" t="1.181"/>\r
+<eng-data cg="53.5" f="17.336" m="42.6813" t="1.263"/>\r
+<eng-data cg="53.5" f="18.009" m="40.1498" t="1.436"/>\r
+<eng-data cg="53.5" f="17.165" m="37.2811" t="1.633"/>\r
+<eng-data cg="53.5" f="17.336" m="35.1243" t="1.784"/>\r
+<eng-data cg="53.5" f="18.682" m="33.9165" t="1.865"/>\r
+<eng-data cg="53.5" f="16.834" m="32.9019" t="1.934"/>\r
+<eng-data cg="53.5" f="17.336" m="32.2371" t="1.981"/>\r
+<eng-data cg="53.5" f="16.332" m="29.4912" t="2.178"/>\r
+<eng-data cg="53.5" f="16.332" m="26.8272" t="2.375"/>\r
+<eng-data cg="53.5" f="18.18" m="25.0126" t="2.502"/>\r
+<eng-data cg="53.5" f="15.659" m="22.7431" t="2.664"/>\r
+<eng-data cg="53.5" f="15.488" m="19.7515" t="2.896"/>\r
+<eng-data cg="53.5" f="13.8" m="14.9742" t="3.29"/>\r
+<eng-data cg="53.5" f="11.611" m="10.4716" t="3.718"/>\r
+<eng-data cg="53.5" f="9.426" m="6.4392" t="4.181"/>\r
+<eng-data cg="53.5" f="5.891" m="1.95597" t="4.888"/>\r
+<eng-data cg="53.5" f="0." m="0." t="5.69"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-F20EJ 29 83 4-7 0.03 0.0746 AeroTech\r
-0.01 52.08\r
-0.03 49.81\r
-0.06 46.98\r
-0.1 45.56\r
-0.15 44.49\r
-0.18 45.55\r
-0.21 43.42\r
-0.24 43.78\r
-0.32 43.77\r
-0.36 44.11\r
-0.44 43.04\r
-0.45 40.58\r
-0.53 39.86\r
-0.62 38.08\r
-0.76 36.3\r
-0.8 37.35\r
-0.84 34.88\r
-0.89 36.99\r
-0.9 33.46\r
-1.03 30.61\r
-1.06 32.02\r
-1.09 29.55\r
-1.23 26\r
-1.32 22.45\r
-1.35 23.16\r
-1.36 21.39\r
-1.58 16.42\r
-1.8 11.1\r
-2.01 6.48\r
-2.19 3.63\r
-2.39 1.13\r
-2.68 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="205.89" Itot="60.573" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="22.602" burn-time="2.68" cgDiv="10" cgFix="1" cgStep="-1." code="F20EJ" delays="4,7" dia="29." exitDia="0." initWt="74.6" len="83." mDiv="10" mFix="1" mStep="-1." massFrac="40.21" mfg="Aerotech" peakThrust="52.08" propWt="30." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="41.5" f="0." m="30." t="0."/>\r
+<eng-data cg="41.5" f="52.08" m="29.871" t="0.01"/>\r
+<eng-data cg="41.5" f="49.81" m="29.3664" t="0.03"/>\r
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+<eng-data cg="41.5" f="45.56" m="27.7307" t="0.1"/>\r
+<eng-data cg="41.5" f="44.49" m="26.6157" t="0.15"/>\r
+<eng-data cg="41.5" f="45.55" m="25.9468" t="0.18"/>\r
+<eng-data cg="41.5" f="43.42" m="25.2859" t="0.21"/>\r
+<eng-data cg="41.5" f="43.78" m="24.6381" t="0.24"/>\r
+<eng-data cg="41.5" f="43.77" m="22.9036" t="0.32"/>\r
+<eng-data cg="41.5" f="44.11" m="22.0331" t="0.36"/>\r
+<eng-data cg="41.5" f="43.04" m="20.3066" t="0.44"/>\r
+<eng-data cg="41.5" f="40.58" m="20.0996" t="0.45"/>\r
+<eng-data cg="41.5" f="39.86" m="18.506" t="0.53"/>\r
+<eng-data cg="41.5" f="38.08" m="16.7689" t="0.62"/>\r
+<eng-data cg="41.5" f="36.3" m="14.1903" t="0.76"/>\r
+<eng-data cg="41.5" f="37.35" m="13.4608" t="0.8"/>\r
+<eng-data cg="41.5" f="34.88" m="12.7453" t="0.84"/>\r
+<eng-data cg="41.5" f="36.99" m="11.8554" t="0.89"/>\r
+<eng-data cg="41.5" f="33.46" m="11.681" t="0.9"/>\r
+<eng-data cg="41.5" f="30.61" m="9.6184" t="1.03"/>\r
+<eng-data cg="41.5" f="32.02" m="9.15312" t="1.06"/>\r
+<eng-data cg="41.5" f="29.55" m="8.69571" t="1.09"/>\r
+<eng-data cg="41.5" f="26." m="6.76986" t="1.23"/>\r
+<eng-data cg="41.5" f="22.45" m="5.69006" t="1.32"/>\r
+<eng-data cg="41.5" f="23.16" m="5.35122" t="1.35"/>\r
+<eng-data cg="41.5" f="21.39" m="5.2409" t="1.36"/>\r
+<eng-data cg="41.5" f="16.42" m="3.18103" t="1.58"/>\r
+<eng-data cg="41.5" f="11.1" m="1.68176" t="1.8"/>\r
+<eng-data cg="41.5" f="6.48" m="0.767541" t="2.01"/>\r
+<eng-data cg="41.5" f="3.63" m="0.316897" t="2.19"/>\r
+<eng-data cg="41.5" f="1.13" m="0.0811496" t="2.39"/>\r
+<eng-data cg="41.5" f="0." m="0." t="2.68"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="189.81" Itot="55.842" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="22.202" burn-time="2.52" cgDiv="10" cgFix="1" cgStep="-1." code="F21W" delays="4,6,8" dia="24." exitDia="0." initWt="64." len="96." mDiv="10" mFix="1" mStep="-1." massFrac="46.88" mfg="Aerotech" peakThrust="42.504" propWt="30." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F21W (White Lightning) RASP.ENG file.\r
+File produced Jun 22 2004.\r
+The file was produced by scaling data points off the\r
+thrust curve in the Tripoli.org motor pdf file.\r
+\r
+The F21W cannot be found on thrustcurve.org.\r
+Hence the amateur file production.\r
+The file was created by Stan Hemphill\r
+Contact at stanley_hemphill@hotmail.com;\r
+</comments>\r
+<data>\r
+<eng-data cg="48." f="0." m="30." t="0."/>\r
+<eng-data cg="48." f="37.2266" m="29.955" t="0.0045"/>\r
+<eng-data cg="48." f="42.1474" m="29.8591" t="0.009"/>\r
+<eng-data cg="48." f="42.504" m="29.6544" t="0.018"/>\r
+<eng-data cg="48." f="40.5071" m="29.4537" t="0.027"/>\r
+<eng-data cg="48." f="38.8669" m="29.3109" t="0.0337"/>\r
+<eng-data cg="48." f="38.225" m="29.1245" t="0.0427"/>\r
+<eng-data cg="48." f="37.7258" m="28.9409" t="0.0517"/>\r
+<eng-data cg="48." f="36.87" m="28.7606" t="0.0607"/>\r
+<eng-data cg="48." f="36.4422" m="28.538" t="0.072"/>\r
+<eng-data cg="48." f="36.4422" m="28.2307" t="0.0877"/>\r
+<eng-data cg="48." f="35.3724" m="27.7966" t="0.1102"/>\r
+<eng-data cg="48." f="35.8716" m="27.322" t="0.135"/>\r
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+<eng-data cg="48." f="38.7242" m="20.5082" t="0.4747"/>\r
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+<eng-data cg="48." f="37.8685" m="17.9343" t="0.6007"/>\r
+<eng-data cg="48." f="36.87" m="17.1674" t="0.6389"/>\r
+<eng-data cg="48." f="37.1553" m="16.5411" t="0.6704"/>\r
+<eng-data cg="48." f="35.9429" m="14.6856" t="0.7649"/>\r
+<eng-data cg="48." f="32.9477" m="11.8136" t="0.9201"/>\r
+<eng-data cg="48." f="30.309" m="10.3608" t="1.0056"/>\r
+<eng-data cg="48." f="29.7385" m="9.30753" t="1.0709"/>\r
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+<eng-data cg="48." f="20.8241" m="4.96627" t="1.3926"/>\r
+<eng-data cg="48." f="15.4754" m="3.05808" t="1.5883"/>\r
+<eng-data cg="48." f="15.4754" m="2.87102" t="1.6108"/>\r
+<eng-data cg="48." f="5.0634" m="0.662014" t="2.0112"/>\r
+<eng-data cg="48." f="3.4231" m="0.415818" t="2.1192"/>\r
+<eng-data cg="48." f="2.4247" m="0.224965" t="2.2407"/>\r
+<eng-data cg="48." f="1.4976" m="0.0803083" t="2.378"/>\r
+<eng-data cg="48." f="0.9271" m="0.00560322" t="2.4927"/>\r
+<eng-data cg="48." f="0." m="0." t="2.5152"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech F22 RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-F22 29 125 4-7 0.0463 0.1342 AT\r
-0.014 11.527\r
-0.075 20.126\r
-0.157 26.572\r
-0.293 29.113\r
-0.382 30.278\r
-0.45 29.69\r
-0.539 30.667\r
-0.614 30.089\r
-0.662 31.15\r
-0.771 30.478\r
-0.948 29.89\r
-0.996 28.714\r
-1.078 28.136\r
-1.187 27.738\r
-1.289 26.761\r
-1.337 26.96\r
-1.412 25.984\r
-1.474 25.008\r
-1.515 26.173\r
-1.542 24.808\r
-1.706 22.856\r
-1.938 20.903\r
-2.101 18.173\r
-2.129 19.338\r
-2.251 16.21\r
-2.402 13.48\r
-2.64 8.791\r
-2.961 3.32\r
-3.31 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="143.15" Itot="64.997" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="19.637" burn-time="3.31" cgDiv="10" cgFix="1" cgStep="-1." code="F22" delays="4,7" dia="29." exitDia="0." initWt="134.2" len="125." mDiv="10" mFix="1" mStep="-1." massFrac="34.5" mfg="Aerotech" peakThrust="31.15" propWt="46.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F22 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="62.5" f="0." m="46.3" t="0."/>\r
+<eng-data cg="62.5" f="11.527" m="46.2425" t="0.014"/>\r
+<eng-data cg="62.5" f="20.126" m="45.5548" t="0.075"/>\r
+<eng-data cg="62.5" f="26.572" m="44.191" t="0.157"/>\r
+<eng-data cg="62.5" f="29.113" m="41.4936" t="0.293"/>\r
+<eng-data cg="62.5" f="30.278" m="39.611" t="0.382"/>\r
+<eng-data cg="62.5" f="29.69" m="38.1586" t="0.45"/>\r
+<eng-data cg="62.5" f="30.667" m="36.2453" t="0.539"/>\r
+<eng-data cg="62.5" f="30.089" m="34.6223" t="0.614"/>\r
+<eng-data cg="62.5" f="31.15" m="33.5754" t="0.662"/>\r
+<eng-data cg="62.5" f="30.478" m="31.1828" t="0.771"/>\r
+<eng-data cg="62.5" f="29.89" m="27.3771" t="0.948"/>\r
+<eng-data cg="62.5" f="28.714" m="26.3752" t="0.996"/>\r
+<eng-data cg="62.5" f="28.136" m="24.7148" t="1.078"/>\r
+<eng-data cg="62.5" f="27.738" m="22.5457" t="1.187"/>\r
+<eng-data cg="62.5" f="26.761" m="20.5658" t="1.289"/>\r
+<eng-data cg="62.5" f="26.96" m="19.6473" t="1.337"/>\r
+<eng-data cg="62.5" f="25.984" m="18.2331" t="1.412"/>\r
+<eng-data cg="62.5" f="25.008" m="17.107" t="1.474"/>\r
+<eng-data cg="62.5" f="26.173" m="16.3596" t="1.515"/>\r
+<eng-data cg="62.5" f="24.808" m="15.8694" t="1.542"/>\r
+<eng-data cg="62.5" f="22.856" m="13.0852" t="1.706"/>\r
+<eng-data cg="62.5" f="20.903" m="9.46934" t="1.938"/>\r
+<eng-data cg="62.5" f="18.173" m="7.20075" t="2.101"/>\r
+<eng-data cg="62.5" f="19.338" m="6.82667" t="2.129"/>\r
+<eng-data cg="62.5" f="16.21" m="5.28201" t="2.251"/>\r
+<eng-data cg="62.5" f="13.48" m="3.68523" t="2.402"/>\r
+<eng-data cg="62.5" f="8.791" m="1.79735" t="2.64"/>\r
+<eng-data cg="62.5" f="3.32" m="0.412687" t="2.961"/>\r
+<eng-data cg="62.5" f="0." m="0." t="3.31"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;F23FJ Motor Thrust Curve created by Tim Van Milligan\r
-;for RockSim Users - www.rocksim.com\r
-;file produced March 2, 2005\r
-;Based on data supplied by Aerotech for the newer molded case F23 econojet.\r
-F23FJ 29 83 4-7 0.033 0.0839 AeroTech\r
-0.03 48.7\r
-0.05 43.11\r
-0.08 41.41\r
-0.1 42.26\r
-0.13 40.84\r
-0.17 39.42\r
-0.23 38.85\r
-0.27 38.85\r
-0.3 37.44\r
-0.31 38.57\r
-0.36 37.72\r
-0.43 36.59\r
-0.5 36.02\r
-0.56 36.02\r
-0.59 34.6\r
-0.69 33.18\r
-0.77 32.61\r
-0.85 31.2\r
-0.94 29.5\r
-1.04 27.79\r
-1.18 24.39\r
-1.2 25.24\r
-1.25 22.97\r
-1.37 20.98\r
-1.53 16.73\r
-1.69 12.48\r
-1.83 9.07\r
-1.95 5.11\r
-2.07 2.27\r
-2.22 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="163.12" Itot="52.787" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="23.778" burn-time="2.22" cgDiv="10" cgFix="1" cgStep="-1." code="F23FJ" delays="4,7" dia="29." exitDia="0." initWt="83.9" len="83." mDiv="10" mFix="1" mStep="-1." massFrac="39.33" mfg="Aerotech" peakThrust="48.7" propWt="33." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>F23FJ Motor Thrust Curve created by Tim Van Milligan\r
+for RockSim Users - www.rocksim.com\r
+file produced March 2, 2005\r
+Based on data supplied by Aerotech for the newer molded case F23 econojet.\r
+</comments>\r
+<data>\r
+<eng-data cg="41.5" f="0." m="33." t="0."/>\r
+<eng-data cg="41.5" f="48.7" m="32.5433" t="0.03"/>\r
+<eng-data cg="41.5" f="43.11" m="31.9694" t="0.05"/>\r
+<eng-data cg="41.5" f="41.41" m="31.1768" t="0.08"/>\r
+<eng-data cg="41.5" f="42.26" m="30.6538" t="0.1"/>\r
+<eng-data cg="41.5" f="40.84" m="29.8745" t="0.13"/>\r
+<eng-data cg="41.5" f="39.42" m="28.871" t="0.17"/>\r
+<eng-data cg="41.5" f="38.85" m="27.4031" t="0.23"/>\r
+<eng-data cg="41.5" f="38.85" m="26.4316" t="0.27"/>\r
+<eng-data cg="41.5" f="37.44" m="25.7162" t="0.3"/>\r
+<eng-data cg="41.5" f="38.57" m="25.4786" t="0.31"/>\r
+<eng-data cg="41.5" f="37.72" m="24.2863" t="0.36"/>\r
+<eng-data cg="41.5" f="36.59" m="22.6604" t="0.43"/>\r
+<eng-data cg="41.5" f="36.02" m="21.0717" t="0.5"/>\r
+<eng-data cg="41.5" f="36.02" m="19.7206" t="0.56"/>\r
+<eng-data cg="41.5" f="34.6" m="19.0584" t="0.59"/>\r
+<eng-data cg="41.5" f="33.18" m="16.9397" t="0.69"/>\r
+<eng-data cg="41.5" f="32.61" m="15.2946" t="0.77"/>\r
+<eng-data cg="41.5" f="31.2" m="13.699" t="0.85"/>\r
+<eng-data cg="41.5" f="29.5" m="11.9914" t="0.94"/>\r
+<eng-data cg="41.5" f="27.79" m="10.2006" t="1.04"/>\r
+<eng-data cg="41.5" f="24.39" m="7.91721" t="1.18"/>\r
+<eng-data cg="41.5" f="25.24" m="7.60695" t="1.2"/>\r
+<eng-data cg="41.5" f="22.97" m="6.85349" t="1.25"/>\r
+<eng-data cg="41.5" f="20.98" m="5.20497" t="1.37"/>\r
+<eng-data cg="41.5" f="16.73" m="3.31901" t="1.53"/>\r
+<eng-data cg="41.5" f="12.48" m="1.85816" t="1.69"/>\r
+<eng-data cg="41.5" f="9.07" m="0.915125" t="1.83"/>\r
+<eng-data cg="41.5" f="5.11" m="0.383248" t="1.95"/>\r
+<eng-data cg="41.5" f="2.27" m="0.106432" t="2.07"/>\r
+<eng-data cg="41.5" f="0." m="0." t="2.22"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech F23RCWSK RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-F23-RC-SK 32 107 100 0.0378 0.1287 AT\r
-0.042 22.644\r
-0.133 28.191\r
-0.161 27.261\r
-0.189 29.57\r
-0.252 31.419\r
-0.343 32.578\r
-0.399 32.348\r
-0.441 33.737\r
-0.476 30.729\r
-0.539 33.507\r
-0.609 34.197\r
-0.777 34.886\r
-0.826 34.656\r
-0.896 36\r
-0.938 34.656\r
-1.015 34.656\r
-1.071 34.197\r
-1.12 33.038\r
-1.218 32.578\r
-1.267 29.81\r
-1.351 29.34\r
-1.393 27.731\r
-1.54 26.802\r
-1.645 24.263\r
-1.799 21.255\r
-1.862 19.866\r
-2.051 15.479\r
-2.317 11.552\r
-2.618 6.7\r
-2.884 3.234\r
-3.185 1.386\r
-3.47 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="181.93" Itot="67.44" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="19.435" burn-time="3.47" cgDiv="10" cgFix="1" cgStep="-1." code="F23-RC-SK" delays="1000" dia="32." exitDia="0." initWt="128.7" len="107." mDiv="10" mFix="1" mStep="-1." massFrac="29.37" mfg="Aerotech" peakThrust="36." propWt="37.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F23RCWSK RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="53.5" f="0." m="37.8" t="0."/>\r
+<eng-data cg="53.5" f="22.644" m="37.5335" t="0.042"/>\r
+<eng-data cg="53.5" f="28.191" m="36.237" t="0.133"/>\r
+<eng-data cg="53.5" f="27.261" m="35.8019" t="0.161"/>\r
+<eng-data cg="53.5" f="29.57" m="35.3559" t="0.189"/>\r
+<eng-data cg="53.5" f="31.419" m="34.2791" t="0.252"/>\r
+<eng-data cg="53.5" f="32.578" m="32.647" t="0.343"/>\r
+<eng-data cg="53.5" f="32.348" m="31.6281" t="0.399"/>\r
+<eng-data cg="53.5" f="33.737" m="30.8502" t="0.441"/>\r
+<eng-data cg="53.5" f="30.729" m="30.2179" t="0.476"/>\r
+<eng-data cg="53.5" f="33.507" m="29.0837" t="0.539"/>\r
+<eng-data cg="53.5" f="34.197" m="27.7556" t="0.609"/>\r
+<eng-data cg="53.5" f="34.886" m="24.503" t="0.777"/>\r
+<eng-data cg="53.5" f="34.656" m="23.548" t="0.826"/>\r
+<eng-data cg="53.5" f="36." m="22.1619" t="0.896"/>\r
+<eng-data cg="53.5" f="34.656" m="21.3302" t="0.938"/>\r
+<eng-data cg="53.5" f="34.656" m="19.8345" t="1.015"/>\r
+<eng-data cg="53.5" f="34.197" m="18.754" t="1.071"/>\r
+<eng-data cg="53.5" f="33.038" m="17.8307" t="1.12"/>\r
+<eng-data cg="53.5" f="32.578" m="16.0286" t="1.218"/>\r
+<eng-data cg="53.5" f="29.81" m="15.1718" t="1.267"/>\r
+<eng-data cg="53.5" f="29.34" m="13.7794" t="1.351"/>\r
+<eng-data cg="53.5" f="27.731" m="13.1076" t="1.393"/>\r
+<eng-data cg="53.5" f="26.802" m="10.861" t="1.54"/>\r
+<eng-data cg="53.5" f="24.263" m="9.35836" t="1.645"/>\r
+<eng-data cg="53.5" f="21.255" m="7.39386" t="1.799"/>\r
+<eng-data cg="53.5" f="19.866" m="6.66784" t="1.862"/>\r
+<eng-data cg="53.5" f="15.479" m="4.7957" t="2.051"/>\r
+<eng-data cg="53.5" f="11.552" m="2.78063" t="2.317"/>\r
+<eng-data cg="53.5" f="6.7" m="1.24097" t="2.618"/>\r
+<eng-data cg="53.5" f="3.234" m="0.500425" t="2.884"/>\r
+<eng-data cg="53.5" f="1.386" m="0.110702" t="3.185"/>\r
+<eng-data cg="53.5" f="0." m="0." t="3.47"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="253.89" Itot="47.306" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="22.209" burn-time="2.13" cgDiv="10" cgFix="1" cgStep="-1." code="F24" delays="4,7" dia="24." exitDia="0." initWt="62.5" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="30.4" mfg="Aerotech" peakThrust="40.95" propWt="19." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F24 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="19." t="0."/>\r
+<eng-data cg="35." f="15.942" m="18.8944" t="0.033"/>\r
+<eng-data cg="35." f="40.146" m="18.0045" t="0.112"/>\r
+<eng-data cg="35." f="40.95" m="17.7928" t="0.125"/>\r
+<eng-data cg="35." f="40.427" m="16.894" t="0.18"/>\r
+<eng-data cg="35." f="40.126" m="15.8425" t="0.245"/>\r
+<eng-data cg="35." f="40.417" m="15.2602" t="0.281"/>\r
+<eng-data cg="35." f="39.524" m="14.0722" t="0.355"/>\r
+<eng-data cg="35." f="39.213" m="12.7598" t="0.438"/>\r
+<eng-data cg="35." f="37.727" m="11.1374" t="0.543"/>\r
+<eng-data cg="35." f="36.532" m="10.2427" t="0.603"/>\r
+<eng-data cg="35." f="33.279" m="9.47159" t="0.658"/>\r
+<eng-data cg="35." f="34.163" m="9.10591" t="0.685"/>\r
+<eng-data cg="35." f="29.434" m="8.58227" t="0.726"/>\r
+<eng-data cg="35." f="29.716" m="8.03586" t="0.772"/>\r
+<eng-data cg="35." f="26.453" m="6.01675" t="0.951"/>\r
+<eng-data cg="35." f="24.666" m="4.78485" t="1.071"/>\r
+<eng-data cg="35." f="22.588" m="4.44323" t="1.107"/>\r
+<eng-data cg="35." f="20.811" m="3.76342" t="1.185"/>\r
+<eng-data cg="35." f="16.644" m="2.27411" t="1.383"/>\r
+<eng-data cg="35." f="10.41" m="0.828926" t="1.649"/>\r
+<eng-data cg="35." f="5.369" m="0.261717" t="1.828"/>\r
+<eng-data cg="35." f="2.403" m="0.0900311" t="1.938"/>\r
+<eng-data cg="35." f="1.806" m="0.0477682" t="1.988"/>\r
+<eng-data cg="35." f="0.912" m="0.0150182" t="2.048"/>\r
+<eng-data cg="35." f="0." m="0." t="2.13"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;F25 Motor Thrust Curve created by Tim Van Milligan\r
-;for RockSim Users - www.rocksim.com\r
-;file produced March 2, 2005\r
-;Based on data supplied by Aerotech for the newer molded case F25.\r
-F25 29 98 4-6-9 0.0388 0.0972 Aerotech\r
-0.039 57.631\r
-0.187 53.491\r
-0.342 51.239\r
-0.5 47.86\r
-1 33.806\r
-1.5 22.94\r
-2 10.135\r
-2.207 4.504\r
-2.69 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="185.98" Itot="70.767" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="26.307" burn-time="2.69" cgDiv="10" cgFix="1" cgStep="-1." code="F25" delays="4,6,9" dia="29." exitDia="0." initWt="97.2" len="98." mDiv="10" mFix="1" mStep="-1." massFrac="39.92" mfg="Aerotech" peakThrust="57.631" propWt="38.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>F25 Motor Thrust Curve created by Tim Van Milligan\r
+for RockSim Users - www.rocksim.com\r
+file produced March 2, 2005\r
+Based on data supplied by Aerotech for the newer molded case F25.\r
+</comments>\r
+<data>\r
+<eng-data cg="49." f="0." m="38.8" t="0."/>\r
+<eng-data cg="49." f="57.631" m="38.1838" t="0.039"/>\r
+<eng-data cg="49." f="53.491" m="33.6753" t="0.187"/>\r
+<eng-data cg="49." f="51.239" m="29.2252" t="0.342"/>\r
+<eng-data cg="49." f="47.86" m="24.9328" t="0.5"/>\r
+<eng-data cg="49." f="33.806" m="13.7388" t="1."/>\r
+<eng-data cg="49." f="22.94" m="5.96068" t="1.5"/>\r
+<eng-data cg="49." f="10.135" m="1.42709" t="2."/>\r
+<eng-data cg="49." f="4.504" m="0.596372" t="2.207"/>\r
+<eng-data cg="49." f="0." m="0." t="2.69"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;F26FJ Motor Thrust Curve created by Tim Van Milligan\r
-;for RockSim Users - www.rocksim.com\r
-;File created March 2, 2005\r
-;Based on data supplied by Aerotech prior to NAR certification.\r
-F26FJ 29 98 6-9 0.0431 0.1007 Aerotech\r
-0.041 38.289\r
-0.114 36.318\r
-0.293 34.347\r
-0.497 32.939\r
-0.774 32.376\r
-1 31.25\r
-1.254 28.716\r
-1.498 25.338\r
-1.743 22.241\r
-2.003 17.737\r
-2.077 15.484\r
-2.304 5.349\r
-2.484 1.689\r
-2.61 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="147.87" Itot="62.501" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="23.947" burn-time="2.61" cgDiv="10" cgFix="1" cgStep="-1." code="F26FJ" delays="6,9" dia="29." exitDia="0." initWt="100.7" len="98." mDiv="10" mFix="1" mStep="-1." massFrac="42.8" mfg="Aerotech" peakThrust="38.289" propWt="43.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>F26FJ Motor Thrust Curve created by Tim Van Milligan\r
+for RockSim Users - www.rocksim.com\r
+File created March 2, 2005\r
+Based on data supplied by Aerotech prior to NAR certification.\r
+</comments>\r
+<data>\r
+<eng-data cg="49." f="0." m="43.1" t="0."/>\r
+<eng-data cg="49." f="38.289" m="42.5587" t="0.041"/>\r
+<eng-data cg="49." f="36.318" m="40.6809" t="0.114"/>\r
+<eng-data cg="49." f="34.347" m="36.3196" t="0.293"/>\r
+<eng-data cg="49." f="32.939" m="31.5868" t="0.497"/>\r
+<eng-data cg="49." f="32.376" m="25.3487" t="0.774"/>\r
+<eng-data cg="49." f="31.25" m="20.3907" t="1."/>\r
+<eng-data cg="49." f="28.716" m="15.139" t="1.254"/>\r
+<eng-data cg="49." f="25.338" m="10.5915" t="1.498"/>\r
+<eng-data cg="49." f="22.241" m="6.57226" t="1.743"/>\r
+<eng-data cg="49." f="17.737" m="2.98837" t="2.003"/>\r
+<eng-data cg="49." f="15.484" m="2.14074" t="2.077"/>\r
+<eng-data cg="49." f="5.349" m="0.510176" t="2.304"/>\r
+<eng-data cg="49." f="1.689" m="0.0733771" t="2.484"/>\r
+<eng-data cg="49." f="0." m="0." t="2.61"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech F32 RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-F32 24 124 5-10-15 0.0377 0.0814 AeroTech\r
-0.025 46.699\r
-0.031 51.846\r
-0.061 55.64\r
-0.085 52.868\r
-0.126 47.37\r
-0.245 45.637\r
-0.34 44.946\r
-0.394 42.873\r
-0.447 42.873\r
-0.572 41.14\r
-0.72 39.408\r
-0.744 40.78\r
-0.786 38.026\r
-1.041 35.592\r
-1.136 33.179\r
-1.177 34.541\r
-1.225 32.818\r
-1.379 31.436\r
-1.474 30.394\r
-1.635 28.311\r
-1.676 27.28\r
-1.694 29.683\r
-1.712 26.929\r
-1.854 25.537\r
-1.943 23.815\r
-2.092 21.051\r
-2.187 18.287\r
-2.276 13.82\r
-2.382 7.281\r
-2.525 2.457\r
-2.72 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Aerotech" code="F32" Type="single-use" dia="24." len="90." initWt="65."\r
+propWt="25.8" delays="4,6,8" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="31.14" peakThrust="58.76" throatDia="0." exitDia="0." Itot="56.924"\r
+burn-time="1.83" massFrac="39.69" Isp="224.98" tDiv="10" tStep="-1." tFix="1"\r
+FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+ <comments>Input by Tim Van Milligan based on NAR Certification document Jan 14, 2009\r
+Created using Thrust Curve Tracer.</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="25.8" cg="45."/>\r
+ <eng-data t="0.028" f="2.636" m="25.7833" cg="45."/>\r
+ <eng-data t="0.035" f="5.891" m="25.7697" cg="45."/>\r
+ <eng-data t="0.054" f="53.488" m="25.5141" cg="45."/>\r
+ <eng-data t="0.061" f="57.364" m="25.3382" cg="45."/>\r
+ <eng-data t="0.068" f="58.76" m="25.154" cg="45."/>\r
+ <eng-data t="0.089" f="58.76" m="24.5947" cg="45."/>\r
+ <eng-data t="0.114" f="55.504" m="23.9474" cg="45."/>\r
+ <eng-data t="0.177" f="51.783" m="22.4156" cg="45."/>\r
+ <eng-data t="0.24" f="49.302" m="20.9724" cg="45."/>\r
+ <eng-data t="0.319" f="47.132" m="19.246" cg="45."/>\r
+ <eng-data t="0.429" f="44.651" m="16.958" cg="45."/>\r
+ <eng-data t="0.545" f="41.86" m="14.6838" cg="45."/>\r
+ <eng-data t="0.611" f="41.55" m="13.4362" cg="45."/>\r
+ <eng-data t="0.627" f="40.465" m="13.1389" cg="45."/>\r
+ <eng-data t="0.676" f="40.155" m="12.2436" cg="45."/>\r
+ <eng-data t="0.772" f="38.76" m="10.5268" cg="45."/>\r
+ <eng-data t="0.904" f="36.744" m="8.26819" cg="45."/>\r
+ <eng-data t="1.005" f="34.884" m="6.62872" cg="45."/>\r
+ <eng-data t="1.119" f="32.403" m="4.89038" cg="45."/>\r
+ <eng-data t="1.212" f="30.543" m="3.56376" cg="45."/>\r
+ <eng-data t="1.277" f="28.527" m="2.69364" cg="45."/>\r
+ <eng-data t="1.298" f="27.597" m="2.42654" cg="45."/>\r
+ <eng-data t="1.322" f="26.512" m="2.13225" cg="45."/>\r
+ <eng-data t="1.338" f="24.961" m="1.94561" cg="45."/>\r
+ <eng-data t="1.385" f="21.55" m="1.45022" cg="45."/>\r
+ <eng-data t="1.445" f="15.969" m="0.940067" cg="45."/>\r
+ <eng-data t="1.51" f="10.543" m="0.549537" cg="45."/>\r
+ <eng-data t="1.597" f="5.581" m="0.231638" cg="45."/>\r
+ <eng-data t="1.676" f="2.636" m="0.0845292" cg="45."/>\r
+ <eng-data t="1.746" f="1.24" m="0.0230427" cg="45."/>\r
+ <eng-data t="1.828" f="0." m="0." cg="45."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech F37 RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-F37 29 99 6-10-14 0.0282 0.1086 AT\r
-0.018 7.251\r
-0.053 13.626\r
-0.088 22.331\r
-0.106 25.227\r
-0.141 26.385\r
-0.183 28.411\r
-0.26 37.685\r
-0.31 41.449\r
-0.422 44.035\r
-0.524 45.183\r
-0.59 46.47\r
-0.682 45.153\r
-0.864 43.386\r
-0.934 40.471\r
-1.042 35.23\r
-1.151 29.699\r
-1.246 25.037\r
-1.354 19.796\r
-1.445 13.397\r
-1.498 7.586\r
-1.54 3.226\r
-1.6 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="183.23" Itot="50.671" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="31.669" burn-time="1.6" cgDiv="10" cgFix="1" cgStep="-1." code="F37" delays="6,10,14" dia="29." exitDia="0." initWt="108.6" len="99." mDiv="10" mFix="1" mStep="-1." massFrac="25.97" mfg="Aerotech" peakThrust="46.47" propWt="28.2" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F37 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="49.5" f="0." m="28.2" t="0."/>\r
+<eng-data cg="49.5" f="7.251" m="28.1637" t="0.018"/>\r
+<eng-data cg="49.5" f="13.626" m="27.9604" t="0.053"/>\r
+<eng-data cg="49.5" f="22.331" m="27.6102" t="0.088"/>\r
+<eng-data cg="49.5" f="25.227" m="27.3719" t="0.106"/>\r
+<eng-data cg="49.5" f="26.385" m="26.8693" t="0.141"/>\r
+<eng-data cg="49.5" f="28.411" m="26.2289" t="0.183"/>\r
+<eng-data cg="49.5" f="37.685" m="24.8127" t="0.26"/>\r
+<eng-data cg="49.5" f="41.449" m="23.7117" t="0.31"/>\r
+<eng-data cg="49.5" f="44.035" m="21.0475" t="0.422"/>\r
+<eng-data cg="49.5" f="45.183" m="18.5152" t="0.524"/>\r
+<eng-data cg="49.5" f="46.47" m="16.8319" t="0.59"/>\r
+<eng-data cg="49.5" f="45.153" m="14.4863" t="0.682"/>\r
+<eng-data cg="49.5" f="43.386" m="10.0023" t="0.864"/>\r
+<eng-data cg="49.5" f="40.471" m="8.3689" t="0.934"/>\r
+<eng-data cg="49.5" f="35.23" m="6.09388" t="1.042"/>\r
+<eng-data cg="49.5" f="29.699" m="4.12452" t="1.151"/>\r
+<eng-data cg="49.5" f="25.037" m="2.67756" t="1.246"/>\r
+<eng-data cg="49.5" f="19.796" m="1.3302" t="1.354"/>\r
+<eng-data cg="49.5" f="13.397" m="0.489683" t="1.445"/>\r
+<eng-data cg="49.5" f="7.586" m="0.180223" t="1.498"/>\r
+<eng-data cg="49.5" f="3.226" m="0.0538612" t="1.54"/>\r
+<eng-data cg="49.5" f="0." m="0." t="1.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="223.07" Itot="49.658" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="37.337" burn-time="1.33" cgDiv="10" cgFix="1" cgStep="-1." code="F39" delays="3,6,9" dia="24." exitDia="0." initWt="60." len="70." mDiv="10" mFix="1" mStep="-1." massFrac="37.83" mfg="Aerotech" peakThrust="59.47" propWt="22.7" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F39 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="22.7" t="0."/>\r
+<eng-data cg="35." f="45.057" m="22.597" t="0.01"/>\r
+<eng-data cg="35." f="54.131" m="22.461" t="0.016"/>\r
+<eng-data cg="35." f="58.321" m="21.6899" t="0.046"/>\r
+<eng-data cg="35." f="59.47" m="20.8015" t="0.079"/>\r
+<eng-data cg="35." f="58.311" m="20.1554" t="0.103"/>\r
+<eng-data cg="35." f="57.253" m="19.4422" t="0.13"/>\r
+<eng-data cg="35." f="55.491" m="18.3599" t="0.172"/>\r
+<eng-data cg="35." f="53.738" m="16.7871" t="0.235"/>\r
+<eng-data cg="35." f="51.271" m="14.723" t="0.321"/>\r
+<eng-data cg="35." f="50.566" m="13.7454" t="0.363"/>\r
+<eng-data cg="35." f="49.509" m="13.1965" t="0.387"/>\r
+<eng-data cg="35." f="50.203" m="12.7179" t="0.408"/>\r
+<eng-data cg="35." f="48.804" m="12.3106" t="0.426"/>\r
+<eng-data cg="35." f="47.746" m="11.7147" t="0.453"/>\r
+<eng-data cg="35." f="47.041" m="11.1298" t="0.48"/>\r
+<eng-data cg="35." f="41.059" m="7.10253" t="0.68"/>\r
+<eng-data cg="35." f="39.649" m="6.43844" t="0.716"/>\r
+<eng-data cg="35." f="38.944" m="5.79176" t="0.752"/>\r
+<eng-data cg="35." f="36.487" m="4.80905" t="0.809"/>\r
+<eng-data cg="35." f="34.382" m="3.98296" t="0.86"/>\r
+<eng-data cg="35." f="33.324" m="3.47228" t="0.893"/>\r
+<eng-data cg="35." f="32.619" m="3.11055" t="0.917"/>\r
+<eng-data cg="35." f="28.752" m="1.94631" t="1."/>\r
+<eng-data cg="35." f="25.247" m="1.02065" t="1.075"/>\r
+<eng-data cg="35." f="22.095" m="0.696033" t="1.105"/>\r
+<eng-data cg="35." f="17.201" m="0.507421" t="1.126"/>\r
+<eng-data cg="35." f="13.001" m="0.383167" t="1.144"/>\r
+<eng-data cg="35." f="8.109" m="0.238419" t="1.174"/>\r
+<eng-data cg="35." f="4.606" m="0.107641" t="1.219"/>\r
+<eng-data cg="35." f="2.5" m="0.0394269" t="1.261"/>\r
+<eng-data cg="35." f="0." m="0." t="1.33"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech F40 RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-F40 29 124 4-7-10 0.04 0.126 AT\r
-0.015 17.776\r
-0.049 41.016\r
-0.089 58.793\r
-0.124 62.9\r
-0.148 65.173\r
-0.183 62.442\r
-0.242 68.07\r
-0.292 60.617\r
-0.321 61.524\r
-0.415 60.617\r
-0.524 58.334\r
-0.741 52.412\r
-0.87 48.314\r
-0.889 49.221\r
-0.914 47.397\r
-1.102 40.109\r
-1.285 33.728\r
-1.492 25.064\r
-1.665 15.952\r
-1.808 8.659\r
-1.942 3.19\r
-2.06 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="199.08" Itot="78.094" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="37.91" burn-time="2.06" cgDiv="10" cgFix="1" cgStep="-1." code="F40" delays="4,7,10" dia="29." exitDia="0." initWt="126." len="124." mDiv="10" mFix="1" mStep="-1." massFrac="31.75" mfg="Aerotech" peakThrust="68.07" propWt="40." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F40 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="62." f="0." m="40." t="0."/>\r
+<eng-data cg="62." f="17.776" m="39.9317" t="0.015"/>\r
+<eng-data cg="62." f="41.016" m="39.4198" t="0.049"/>\r
+<eng-data cg="62." f="58.793" m="38.3973" t="0.089"/>\r
+<eng-data cg="62." f="62.9" m="37.3065" t="0.124"/>\r
+<eng-data cg="62." f="65.173" m="36.5193" t="0.148"/>\r
+<eng-data cg="62." f="62.442" m="35.3754" t="0.183"/>\r
+<eng-data cg="62." f="68.07" m="33.4034" t="0.242"/>\r
+<eng-data cg="62." f="60.617" m="31.7556" t="0.292"/>\r
+<eng-data cg="62." f="61.524" m="30.8484" t="0.321"/>\r
+<eng-data cg="62." f="60.617" m="27.908" t="0.415"/>\r
+<eng-data cg="62." f="58.334" m="24.5875" t="0.524"/>\r
+<eng-data cg="62." f="52.412" m="18.4329" t="0.741"/>\r
+<eng-data cg="62." f="48.314" m="15.1052" t="0.87"/>\r
+<eng-data cg="62." f="49.221" m="14.6306" t="0.889"/>\r
+<eng-data cg="62." f="47.397" m="14.012" t="0.914"/>\r
+<eng-data cg="62." f="40.109" m="9.79883" t="1.102"/>\r
+<eng-data cg="62." f="33.728" m="6.33834" t="1.285"/>\r
+<eng-data cg="62." f="25.064" m="3.22159" t="1.492"/>\r
+<eng-data cg="62." f="15.952" m="1.40435" t="1.665"/>\r
+<eng-data cg="62." f="8.659" m="0.503032" t="1.808"/>\r
+<eng-data cg="62." f="3.19" m="0.0964019" t="1.942"/>\r
+<eng-data cg="62." f="0." m="0." t="2.06"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;F42T Motor Thrust Curve created by Tim Van Milligan\r
-;for RockSim Users - www.rocksim.com\r
-;Based on data supplied by Aerotech prior to NAR certification.\r
-F42T 29 83 4-8 0.027 0.076 Aerotech\r
-0.01 68.694\r
-0.029 65.879\r
-0.202 62.5\r
-0.511 51.802\r
-0.739 43.356\r
-0.993 31.532\r
-1.02 29.279\r
-1.072 23.086\r
-1.199 9.572\r
-1.262 4.505\r
-1.319 2.815\r
-1.47 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="210.99" Itot="55.866" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="38.004" burn-time="1.47" cgDiv="10" cgFix="1" cgStep="-1." code="F42T" delays="4,8" dia="29." exitDia="0." initWt="76." len="83." mDiv="10" mFix="1" mStep="-1." massFrac="35.53" mfg="Aerotech" peakThrust="68.694" propWt="27." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>F42T Motor Thrust Curve created by Tim Van Milligan\r
+for RockSim Users - www.rocksim.com\r
+Based on data supplied by Aerotech prior to NAR certification.\r
+</comments>\r
+<data>\r
+<eng-data cg="41.5" f="0." m="27." t="0."/>\r
+<eng-data cg="41.5" f="68.694" m="26.834" t="0.01"/>\r
+<eng-data cg="41.5" f="65.879" m="26.2161" t="0.029"/>\r
+<eng-data cg="41.5" f="62.5" m="20.8492" t="0.202"/>\r
+<eng-data cg="41.5" f="51.802" m="12.3143" t="0.511"/>\r
+<eng-data cg="41.5" f="43.356" m="7.07144" t="0.739"/>\r
+<eng-data cg="41.5" f="31.532" m="2.47488" t="0.993"/>\r
+<eng-data cg="41.5" f="29.279" m="2.07812" t="1.02"/>\r
+<eng-data cg="41.5" f="23.086" m="1.42011" t="1.072"/>\r
+<eng-data cg="41.5" f="9.572" m="0.41785" t="1.199"/>\r
+<eng-data cg="41.5" f="4.505" m="0.203543" t="1.262"/>\r
+<eng-data cg="41.5" f="2.815" m="0.102717" t="1.319"/>\r
+<eng-data cg="41.5" f="0." m="0." t="1.47"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech F50 RASP.ENG file made by Tim Van Milligan\r
-;For RockSim www.RockSim.com\r
-;File Created March 2, 2005\r
-;Thrust curve supplied by Aerotech for the molded case F50T motors.\r
-F50T 29 98 4-6-9 0.0336 0.0898 AeroTech\r
-0.013 73.762\r
-0.0326 70.383\r
-0.267 69.82\r
-0.518 67.005\r
-0.792 56.87\r
-0.906 50.676\r
-1 44.482\r
-1.036 39.978\r
-1.107 23.649\r
-1.199 6.194\r
-1.316 1.126\r
-1.43 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="208.54" Itot="68.713" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="48.051" burn-time="1.43" cgDiv="10" cgFix="1" cgStep="-1." code="F50T" delays="4,6,9" dia="29." exitDia="0." initWt="89.8" len="98." mDiv="10" mFix="1" mStep="-1." massFrac="37.42" mfg="Aerotech" peakThrust="73.762" propWt="33.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F50 RASP.ENG file made by Tim Van Milligan\r
+For RockSim www.RockSim.com\r
+File Created March 2, 2005\r
+Thrust curve supplied by Aerotech for the molded case F50T motors.\r
+</comments>\r
+<data>\r
+<eng-data cg="49." f="0." m="33.6" t="0."/>\r
+<eng-data cg="49." f="73.762" m="33.3656" t="0.013"/>\r
+<eng-data cg="49." f="70.383" m="32.6748" t="0.0326"/>\r
+<eng-data cg="49." f="69.82" m="24.6398" t="0.267"/>\r
+<eng-data cg="49." f="67.005" m="16.2431" t="0.518"/>\r
+<eng-data cg="49." f="56.87" m="7.94451" t="0.792"/>\r
+<eng-data cg="49." f="50.676" m="4.94694" t="0.906"/>\r
+<eng-data cg="49." f="44.482" m="2.75997" t="1."/>\r
+<eng-data cg="49." f="39.978" m="2.01657" t="1.036"/>\r
+<eng-data cg="49." f="23.649" m="0.912055" t="1.107"/>\r
+<eng-data cg="49." f="6.194" m="0.24078" t="1.199"/>\r
+<eng-data cg="49." f="1.126" m="0.0313844" t="1.316"/>\r
+<eng-data cg="49." f="0." m="0." t="1.43"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech F52 RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-F52 29 124 5-8-11 0.0366 0.1214 AT\r
-0.012 46.899\r
-0.033 61.778\r
-0.056 69.441\r
-0.097 73.483\r
-0.115 76.636\r
-0.13 74.381\r
-0.153 74.82\r
-0.168 78.422\r
-0.182 78.95\r
-0.206 77.963\r
-0.238 77.504\r
-0.258 73.892\r
-0.314 72.974\r
-0.39 72.046\r
-0.428 70.679\r
-0.501 65.699\r
-0.565 62.975\r
-0.688 58.874\r
-0.749 56.15\r
-0.837 52.517\r
-0.901 49.793\r
-0.971 46.161\r
-1.088 39.365\r
-1.144 34.386\r
-1.173 29.417\r
-1.222 20.376\r
-1.275 13.151\r
-1.339 5.461\r
-1.389 1.838\r
-1.42 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="203.25" Itot="72.95" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="51.374" burn-time="1.42" cgDiv="10" cgFix="1" cgStep="-1." code="F52" delays="5,8,11" dia="29." exitDia="0." initWt="121.4" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="30.15" mfg="Aerotech" peakThrust="78.95" propWt="36.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F52 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="62." f="0." m="36.6" t="0."/>\r
+<eng-data cg="62." f="46.899" m="36.4588" t="0.012"/>\r
+<eng-data cg="62." f="61.778" m="35.8863" t="0.033"/>\r
+<eng-data cg="62." f="69.441" m="35.1292" t="0.056"/>\r
+<eng-data cg="62." f="73.483" m="33.6592" t="0.097"/>\r
+<eng-data cg="62." f="76.636" m="32.9814" t="0.115"/>\r
+<eng-data cg="62." f="74.381" m="32.4131" t="0.13"/>\r
+<eng-data cg="62." f="74.82" m="31.5523" t="0.153"/>\r
+<eng-data cg="62." f="78.422" m="30.9757" t="0.168"/>\r
+<eng-data cg="62." f="78.95" m="30.423" t="0.182"/>\r
+<eng-data cg="62." f="77.963" m="29.4783" t="0.206"/>\r
+<eng-data cg="62." f="77.504" m="28.2303" t="0.238"/>\r
+<eng-data cg="62." f="73.892" m="27.4707" t="0.258"/>\r
+<eng-data cg="62." f="72.974" m="25.4076" t="0.314"/>\r
+<eng-data cg="62." f="72.046" m="22.6428" t="0.39"/>\r
+<eng-data cg="62." f="70.679" m="21.2822" t="0.428"/>\r
+<eng-data cg="62." f="65.699" m="18.7848" t="0.501"/>\r
+<eng-data cg="62." f="62.975" m="16.719" t="0.565"/>\r
+<eng-data cg="62." f="58.874" m="12.9593" t="0.688"/>\r
+<eng-data cg="62." f="56.15" m="11.1992" t="0.749"/>\r
+<eng-data cg="62." f="52.517" m="8.80035" t="0.837"/>\r
+<eng-data cg="62." f="49.793" m="7.15779" t="0.901"/>\r
+<eng-data cg="62." f="46.161" m="5.47285" t="0.971"/>\r
+<eng-data cg="62." f="39.365" m="2.96266" t="1.088"/>\r
+<eng-data cg="62." f="34.386" m="1.92661" t="1.144"/>\r
+<eng-data cg="62." f="29.417" m="1.46246" t="1.173"/>\r
+<eng-data cg="62." f="20.376" m="0.850406" t="1.222"/>\r
+<eng-data cg="62." f="13.151" m="0.404654" t="1.275"/>\r
+<eng-data cg="62." f="5.461" m="0.105843" t="1.339"/>\r
+<eng-data cg="62." f="1.838" m="0.0142932" t="1.389"/>\r
+<eng-data cg="62." f="0." m="0." t="1.42"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Aerotech F62T (Blue Thunder)\r
-;\r
-; AeroTech RMS-29/60 Easy Access Reloadable Motor Hardware.\r
-;\r
-; RASP.ENG file made from manufacturers catalog data.\r
-;\r
-; File produced May, 17 2004.\r
-;\r
-; The file was produced by scaling 16 data points off\r
-; the thrust curves in the manufacturers catalog.\r
-;\r
-; The F62T cannot be found on thrustcurve.org.\r
-; Hence the amateur file production.\r
-; The file was created by Stan Hemphill.\r
-; Contact at stanley_hemphill@hotmail.com.\r
-;\r
-; Motor Dia Len Delay Prop Gross Mfg\r
-F62T 29 99 6-8-9-10-11-13-14-16-18 0.025 0.109 AT\r
-0.0046 053.6364\r
-0.0416 055.2727\r
-0.0909 058.3636\r
-0.1356 061.6364\r
-0.1649 064.9091\r
-0.1864 067.6364\r
-0.5085 067.6364\r
-0.5701 064.7273\r
-0.6687 060.0000\r
-0.7427 055.0909\r
-0.7982 049.6364\r
-0.9029 048.7273\r
-0.9492 024.7273\r
-0.9661 020.1818\r
-0.9985 000.0000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="208.02" Itot="50.998" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="50.998" burn-time="1." cgDiv="10" cgFix="1" cgStep="-1." code="F62T" delays="6,10,14" dia="29." exitDia="0." initWt="109." len="99." mDiv="10" mFix="1" mStep="-1." massFrac="22.94" mfg="Aerotech" peakThrust="59.51" propWt="25." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="49.5" f="0." m="25." t="0."/>\r
+<eng-data cg="49.5" f="47.82" m="25." t="0."/>\r
+<eng-data cg="49.5" f="59.51" m="19.7386" t="0.2"/>\r
+<eng-data cg="49.5" f="59.51" m="10.9868" t="0.5"/>\r
+<eng-data cg="49.5" f="55.56" m="8.16642" t="0.6"/>\r
+<eng-data cg="49.5" f="51.55" m="5.54109" t="0.7"/>\r
+<eng-data cg="49.5" f="43.63" m="3.20818" t="0.8"/>\r
+<eng-data cg="49.5" f="43.63" m="1.06939" t="0.9"/>\r
+<eng-data cg="49.5" f="0." m="0." t="1."/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech F72 RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-F72 24 124 5-10-15 0.0368 0.0742 AeroTech\r
-0.012 62.586\r
-0.017 84.986\r
-0.02 98.78\r
-0.03 94.748\r
-0.05 90.152\r
-0.069 82.688\r
-0.089 85.556\r
-0.104 80.39\r
-0.136 83.255\r
-0.146 80.96\r
-0.176 82.688\r
-0.198 78.672\r
-0.213 80.96\r
-0.253 80.39\r
-0.315 80.96\r
-0.38 79.821\r
-0.429 79.241\r
-0.489 78.092\r
-0.523 78.672\r
-0.536 75.225\r
-0.675 73.496\r
-0.699 67.182\r
-0.719 68.331\r
-0.747 64.884\r
-0.769 66.033\r
-0.858 60.867\r
-0.923 52.824\r
-0.98 40.195\r
-1.012 29.864\r
-1.034 20.092\r
-1.089 11.48\r
-1.21 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="207.6" Itot="74.919" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="61.917" burn-time="1.21" cgDiv="10" cgFix="1" cgStep="-1." code="F72" delays="5,10,15" dia="24." exitDia="0." initWt="74.2" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="49.6" mfg="Aerotech" peakThrust="98.78" propWt="36.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F72 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="62." f="0." m="36.8" t="0."/>\r
+<eng-data cg="62." f="62.586" m="36.6155" t="0.012"/>\r
+<eng-data cg="62." f="84.986" m="36.4343" t="0.017"/>\r
+<eng-data cg="62." f="98.78" m="36.2989" t="0.02"/>\r
+<eng-data cg="62." f="94.748" m="35.8236" t="0.03"/>\r
+<eng-data cg="62." f="90.152" m="34.9154" t="0.05"/>\r
+<eng-data cg="62." f="82.688" m="34.1089" t="0.069"/>\r
+<eng-data cg="62." f="85.556" m="33.2825" t="0.089"/>\r
+<eng-data cg="62." f="80.39" m="32.6711" t="0.104"/>\r
+<eng-data cg="62." f="83.255" m="31.385" t="0.136"/>\r
+<eng-data cg="62." f="80.96" m="30.9817" t="0.146"/>\r
+<eng-data cg="62." f="82.688" m="29.776" t="0.176"/>\r
+<eng-data cg="62." f="78.672" m="28.9041" t="0.198"/>\r
+<eng-data cg="62." f="80.96" m="28.3161" t="0.213"/>\r
+<eng-data cg="62." f="80.39" m="26.731" t="0.253"/>\r
+<eng-data cg="62." f="80.96" m="24.2741" t="0.315"/>\r
+<eng-data cg="62." f="79.821" m="21.7074" t="0.38"/>\r
+<eng-data cg="62." f="79.241" m="19.7932" t="0.429"/>\r
+<eng-data cg="62." f="78.092" m="17.4748" t="0.489"/>\r
+<eng-data cg="62." f="78.672" m="16.1657" t="0.523"/>\r
+<eng-data cg="62." f="75.225" m="15.6744" t="0.536"/>\r
+<eng-data cg="62." f="73.496" m="10.5973" t="0.675"/>\r
+<eng-data cg="62." f="67.182" m="9.76815" t="0.699"/>\r
+<eng-data cg="62." f="68.331" m="9.10251" t="0.719"/>\r
+<eng-data cg="62." f="64.884" m="8.18643" t="0.747"/>\r
+<eng-data cg="62." f="66.033" m="7.47907" t="0.769"/>\r
+<eng-data cg="62." f="60.867" m="4.70527" t="0.858"/>\r
+<eng-data cg="62." f="52.824" m="2.89032" t="0.923"/>\r
+<eng-data cg="62." f="40.195" m="1.58815" t="0.98"/>\r
+<eng-data cg="62." f="29.864" m="1.03754" t="1.012"/>\r
+<eng-data cg="62." f="20.092" m="0.767624" t="1.034"/>\r
+<eng-data cg="62." f="11.48" m="0.341154" t="1.089"/>\r
+<eng-data cg="62." f="0." m="0." t="1.21"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; Aerotech G104T (Blue Thunder)\r
-;\r
-; AeroTech RMS-29/100 EZ Access Reloadable Motors.\r
-;\r
-; File produced 28 Feb 2005.\r
-;\r
-; The file was produced by scaling data points off the\r
-; thrust curve in the manufacturers catalog sheet.\r
-;\r
-; The motor is not yet on www.thrustcurve.org.\r
-; Hence the amateur file production.\r
-; The file was created by Stan Hemphill.\r
-; Contact at stanley_hemphill@hotmail.com.\r
-;\r
-; Motor Dia Len Delay Prop Gross Mfg\r
-G104T 29 124 6-8-9-10-11-13-14-16-18 0.0408 0.136 AT\r
-0.0067 125.3426\r
-0.0471 123.5424\r
-0.0856 121.9671\r
-0.1019 121.4046\r
-0.1462 121.1795\r
-0.1837 120.8420\r
-0.2029 120.5044\r
-0.2385 118.8167\r
-0.2644 117.2415\r
-0.2798 116.9039\r
-0.3279 116.6789\r
-0.3923 116.6789\r
-0.4298 116.1163\r
-0.4615 114.0910\r
-0.5067 110.1530\r
-0.5404 104.6397\r
-0.5760 096.2010\r
-0.6067 089.5626\r
-0.6817 078.8736\r
-0.7692 067.9595\r
-0.7865 064.9216\r
-0.7990 062.5588\r
-0.8058 058.0582\r
-0.8192 050.5196\r
-0.8385 039.0430\r
-0.8625 027.5664\r
-0.8769 016.6523\r
-0.9019 000.0000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="207.1" Itot="82.862" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="92.069" burn-time="0.9" cgDiv="10" cgFix="1" cgStep="-1." code="G104T" delays="6,10,14" dia="29." exitDia="0." initWt="135.6" len="125." mDiv="10" mFix="1" mStep="-1." massFrac="30.09" mfg="Aerotech" peakThrust="118.5" propWt="40.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="62.5" f="0." m="40.8" t="0."/>\r
+<eng-data cg="62.5" f="118.5" m="40.8" t="0."/>\r
+<eng-data cg="62.5" f="114.14" m="35.0726" t="0.1"/>\r
+<eng-data cg="62.5" f="114.14" m="29.4525" t="0.2"/>\r
+<eng-data cg="62.5" f="109.91" m="23.9366" t="0.3"/>\r
+<eng-data cg="62.5" f="109.91" m="18.5248" t="0.4"/>\r
+<eng-data cg="62.5" f="105.68" m="13.2171" t="0.5"/>\r
+<eng-data cg="62.5" f="84.56" m="8.53352" t="0.6"/>\r
+<eng-data cg="62.5" f="71.83" m="4.68332" t="0.7"/>\r
+<eng-data cg="62.5" f="59.2" m="1.45746" t="0.8"/>\r
+<eng-data cg="62.5" f="0." m="0." t="0.9"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech G12RC RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-G12RC 32 107 100 0.0511 0.131 AT\r
-0.03 18.549\r
-0.117 19.96\r
-0.239 20.64\r
-0.362 20.111\r
-0.519 18.982\r
-0.694 17.138\r
-0.886 15.02\r
-1.131 13.186\r
-1.375 11.915\r
-1.689 11.069\r
-2.021 10.363\r
-2.422 10.232\r
-3.172 9.677\r
-4.114 9.267\r
-5.039 8.857\r
-6.137 8.733\r
-7.132 8.607\r
-7.795 8.335\r
-7.952 8.196\r
-8.074 8.055\r
-8.179 6.924\r
-8.319 4.661\r
-8.476 1.973\r
-8.55 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="174.04" Itot="87.216" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="10.201" burn-time="8.55" cgDiv="10" cgFix="1" cgStep="-1." code="G12RC" delays="1000" dia="32." exitDia="0." initWt="131." len="107." mDiv="10" mFix="1" mStep="-1." massFrac="39.01" mfg="Aerotech" peakThrust="20.64" propWt="51.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech G12RC RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="53.5" f="0." m="51.1" t="0."/>\r
+<eng-data cg="53.5" f="18.549" m="50.937" t="0.03"/>\r
+<eng-data cg="53.5" f="19.96" m="49.9555" t="0.117"/>\r
+<eng-data cg="53.5" f="20.64" m="48.5045" t="0.239"/>\r
+<eng-data cg="53.5" f="20.111" m="47.0361" t="0.362"/>\r
+<eng-data cg="53.5" f="18.982" m="45.2381" t="0.519"/>\r
+<eng-data cg="53.5" f="17.138" m="43.3864" t="0.694"/>\r
+<eng-data cg="53.5" f="15.02" m="41.5776" t="0.886"/>\r
+<eng-data cg="53.5" f="13.186" m="39.5532" t="1.131"/>\r
+<eng-data cg="53.5" f="11.915" m="37.759" t="1.375"/>\r
+<eng-data cg="53.5" f="11.069" m="35.6448" t="1.689"/>\r
+<eng-data cg="53.5" f="10.363" m="33.5603" t="2.021"/>\r
+<eng-data cg="53.5" f="10.232" m="31.141" t="2.422"/>\r
+<eng-data cg="53.5" f="9.677" m="26.7667" t="3.172"/>\r
+<eng-data cg="53.5" f="9.267" m="21.539" t="4.114"/>\r
+<eng-data cg="53.5" f="8.857" m="16.6278" t="5.039"/>\r
+<eng-data cg="53.5" f="8.733" m="10.9698" t="6.137"/>\r
+<eng-data cg="53.5" f="8.607" m="5.91546" t="7.132"/>\r
+<eng-data cg="53.5" f="8.335" m="2.62489" t="7.795"/>\r
+<eng-data cg="53.5" f="8.196" m="1.86458" t="7.952"/>\r
+<eng-data cg="53.5" f="8.055" m="1.28377" t="8.074"/>\r
+<eng-data cg="53.5" f="6.924" m="0.823023" t="8.179"/>\r
+<eng-data cg="53.5" f="4.661" m="0.347889" t="8.319"/>\r
+<eng-data cg="53.5" f="1.973" m="0.0427712" t="8.476"/>\r
+<eng-data cg="53.5" f="0." m="0." t="8.55"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+; @File: G142_Typical.txt, @Pts-I: 451, @Pts-O: 32, @Sm: 0, @CO: 5% \r
+; @TI: 84.5422, @TIa: 84.2303, @TIe: 0.0%, @ThMax: 173.4408, @ThAvg: 135.8554, @Tb: 0.62 \r
+; Exported using ThrustCurveTool, www.ThrustGear.com \r
+G142 29 113 6-10-14 0.0386 0.0976 Aerotech \r
+ 0.016 4.06052 \r
+ 0.018 6.53754 \r
+ 0.02 13.44075 \r
+ 0.022 24.4211 \r
+ 0.024 43.7388 \r
+ 0.026 72.8495 \r
+ 0.028 106.9426 \r
+ 0.03 132.0076 \r
+ 0.032 141.5423 \r
+ 0.034 147.6844 \r
+ 0.038 154.1148 \r
+ 0.054 165.5675 \r
+ 0.076 166.3214 \r
+ 0.084 168.7605 \r
+ 0.118 172.9402 \r
+ 0.15 173.3837 \r
+ 0.224 171.8426 \r
+ 0.3 164.7803 \r
+ 0.372 156.6537 \r
+ 0.418 148.9594 \r
+ 0.432 144.9903 \r
+ 0.452 137.0965 \r
+ 0.518 96.8779 \r
+ 0.568 69.3937 \r
+ 0.576 63.1618 \r
+ 0.618 21.4754 \r
+ 0.628 13.57047 \r
+ 0.64 7.98504 \r
+ 0.652 2.92169 \r
+ 0.672 0.966347 \r
+ 0.9 0.687625 \r
+ 0.901 0\r
+++ /dev/null
-;\r
-;Aerotech G25 RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-G25 29 124 5-10-15 0.0625 0.1197 AeroTech\r
-0.035 30.499\r
-0.047 36.712\r
-0.059 41.18\r
-0.13 40.669\r
-0.177 38.969\r
-0.295 38.969\r
-0.343 40.947\r
-0.413 40.38\r
-0.437 38.69\r
-0.484 39.824\r
-0.532 37.845\r
-0.65 37.557\r
-0.721 38.969\r
-0.803 38.69\r
-0.85 37.279\r
-0.98 39.535\r
-1.063 36.434\r
-1.098 38.124\r
-1.252 37.845\r
-1.37 37.279\r
-1.583 37\r
-1.819 35.3\r
-1.984 33.61\r
-2.185 31.344\r
-2.315 28.809\r
-2.622 24.286\r
-3.024 18.917\r
-3.39 13.838\r
-3.839 7.624\r
-4.323 4.518\r
-4.783 2.541\r
-5.3 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="191.71" Itot="117.499" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="22.17" burn-time="5.3" cgDiv="10" cgFix="1" cgStep="-1." code="G25" delays="5,10,15" dia="29." exitDia="0." initWt="119.7" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="52.21" mfg="Aerotech" peakThrust="41.18" propWt="62.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech G25 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="62." f="0." m="62.5" t="0."/>\r
+<eng-data cg="62." f="30.499" m="62.2161" t="0.035"/>\r
+<eng-data cg="62." f="36.712" m="62.0016" t="0.047"/>\r
+<eng-data cg="62." f="41.18" m="61.753" t="0.059"/>\r
+<eng-data cg="62." f="40.669" m="60.2074" t="0.13"/>\r
+<eng-data cg="62." f="38.969" m="59.212" t="0.177"/>\r
+<eng-data cg="62." f="38.969" m="56.766" t="0.295"/>\r
+<eng-data cg="62." f="40.947" m="55.7458" t="0.343"/>\r
+<eng-data cg="62." f="40.38" m="54.2317" t="0.413"/>\r
+<eng-data cg="62." f="38.69" m="53.727" t="0.437"/>\r
+<eng-data cg="62." f="39.824" m="52.7456" t="0.484"/>\r
+<eng-data cg="62." f="37.845" m="51.7541" t="0.532"/>\r
+<eng-data cg="62." f="37.557" m="49.3877" t="0.65"/>\r
+<eng-data cg="62." f="38.969" m="47.9427" t="0.721"/>\r
+<eng-data cg="62." f="38.69" m="46.249" t="0.803"/>\r
+<eng-data cg="62." f="37.279" m="45.2994" t="0.85"/>\r
+<eng-data cg="62." f="39.535" m="42.6436" t="0.98"/>\r
+<eng-data cg="62." f="36.434" m="40.9666" t="1.063"/>\r
+<eng-data cg="62." f="38.124" m="40.2726" t="1.098"/>\r
+<eng-data cg="62." f="37.845" m="37.1611" t="1.252"/>\r
+<eng-data cg="62." f="37.279" m="34.8034" t="1.37"/>\r
+<eng-data cg="62." f="37." m="30.5956" t="1.583"/>\r
+<eng-data cg="62." f="35.3" m="26.0576" t="1.819"/>\r
+<eng-data cg="62." f="33.61" m="23.0336" t="1.984"/>\r
+<eng-data cg="62." f="31.344" m="19.5613" t="2.185"/>\r
+<eng-data cg="62." f="28.809" m="17.4815" t="2.315"/>\r
+<eng-data cg="62." f="24.286" m="13.1463" t="2.622"/>\r
+<eng-data cg="62." f="18.917" m="8.52727" t="3.024"/>\r
+<eng-data cg="62." f="13.838" m="5.33886" t="3.39"/>\r
+<eng-data cg="62." f="7.624" m="2.77596" t="3.839"/>\r
+<eng-data cg="62." f="4.518" m="1.213" t="4.323"/>\r
+<eng-data cg="62." f="2.541" m="0.34939" t="4.783"/>\r
+<eng-data cg="62." f="0." m="0." t="5.3"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech G33 RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-G33 29 124 5-7 0.0722 0.1593 AT\r
-0.027 22.642\r
-0.061 42.201\r
-0.117 47.354\r
-0.243 46.678\r
-0.34 46.339\r
-0.438 47.384\r
-0.48 50.92\r
-0.508 46.359\r
-0.543 47.732\r
-0.662 45.693\r
-0.851 42.28\r
-1.039 41.266\r
-1.116 42.987\r
-1.193 39.226\r
-1.221 42.31\r
-1.312 38.888\r
-1.326 40.609\r
-1.479 38.221\r
-1.675 35.157\r
-1.843 32.77\r
-1.878 36.888\r
-1.899 32.093\r
-1.997 30.382\r
-2.13 26.622\r
-2.263 23.547\r
-2.444 19.11\r
-2.591 13.977\r
-2.752 8.502\r
-2.892 4.743\r
-3.053 2.014\r
-3.27 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="138.97" Itot="98.394" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="30.09" burn-time="3.27" cgDiv="10" cgFix="1" cgStep="-1." code="G33" delays="5,7" dia="29." exitDia="0." initWt="159.3" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="45.32" mfg="Aerotech" peakThrust="50.92" propWt="72.2" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech G33 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="62." f="0." m="72.2" t="0."/>\r
+<eng-data cg="62." f="22.642" m="71.9757" t="0.027"/>\r
+<eng-data cg="62." f="42.201" m="71.1668" t="0.061"/>\r
+<eng-data cg="62." f="47.354" m="69.3268" t="0.117"/>\r
+<eng-data cg="62." f="46.678" m="64.9799" t="0.243"/>\r
+<eng-data cg="62." f="46.339" m="61.6695" t="0.34"/>\r
+<eng-data cg="62." f="47.384" m="58.2997" t="0.438"/>\r
+<eng-data cg="62." f="50.92" m="56.7848" t="0.48"/>\r
+<eng-data cg="62." f="46.359" m="55.7855" t="0.508"/>\r
+<eng-data cg="62." f="47.732" m="54.5772" t="0.543"/>\r
+<eng-data cg="62." f="45.693" m="50.4983" t="0.662"/>\r
+<eng-data cg="62." f="42.28" m="44.398" t="0.851"/>\r
+<eng-data cg="62." f="41.266" m="38.6353" t="1.039"/>\r
+<eng-data cg="62." f="42.987" m="36.2551" t="1.116"/>\r
+<eng-data cg="62." f="39.226" m="33.9325" t="1.193"/>\r
+<eng-data cg="62." f="42.31" m="33.0949" t="1.221"/>\r
+<eng-data cg="62." f="38.888" m="30.3839" t="1.312"/>\r
+<eng-data cg="62." f="40.609" m="29.9756" t="1.326"/>\r
+<eng-data cg="62." f="38.221" m="25.5505" t="1.479"/>\r
+<eng-data cg="62." f="35.157" m="20.2738" t="1.675"/>\r
+<eng-data cg="62." f="32.77" m="16.0869" t="1.843"/>\r
+<eng-data cg="62." f="36.888" m="15.1924" t="1.878"/>\r
+<eng-data cg="62." f="32.093" m="14.6609" t="1.899"/>\r
+<eng-data cg="62." f="30.382" m="12.4146" t="1.997"/>\r
+<eng-data cg="62." f="26.622" m="9.63298" t="2.13"/>\r
+<eng-data cg="62." f="23.547" m="7.18489" t="2.263"/>\r
+<eng-data cg="62." f="19.11" m="4.35213" t="2.444"/>\r
+<eng-data cg="62." f="13.977" m="2.56764" t="2.591"/>\r
+<eng-data cg="62." f="8.502" m="1.23981" t="2.752"/>\r
+<eng-data cg="62." f="4.743" m="0.559481" t="2.892"/>\r
+<eng-data cg="62." f="2.014" m="0.160346" t="3.053"/>\r
+<eng-data cg="62." f="0." m="0." t="3.27"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; 38-120\r
-; Created from TRA Certification Record issued 23 Nov 2006\r
-; Bill Wagstaff - 04/30/07\r
-G339N 38 97 0 0.049 0.190 AT\r
-0.009 371\r
-0.05 375\r
-0.10 375\r
-0.15 364\r
-0.20 349\r
-0.25 310\r
-0.30 264\r
-0.324 257\r
-0.342 39\r
-0.359 0\r
-;\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="233.25" Itot="112.085" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="312.214" burn-time="0.36" cgDiv="10" cgFix="1" cgStep="-1." code="G339N" delays="100" dia="38." exitDia="0." initWt="190." len="97." mDiv="10" mFix="1" mStep="-1." massFrac="25.79" mfg="Aerotech" peakThrust="375." propWt="49." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Created from TRA Certification Record issued 23 Nov 2006\r
+Bill Wagstaff - 04/30/07\r
+</comments>\r
+<data>\r
+<eng-data cg="48.5" f="0." m="49." t="0."/>\r
+<eng-data cg="48.5" f="371." m="48.2701" t="0.009"/>\r
+<eng-data cg="48.5" f="375." m="41.5845" t="0.05"/>\r
+<eng-data cg="48.5" f="375." m="33.3876" t="0.1"/>\r
+<eng-data cg="48.5" f="364." m="25.3109" t="0.15"/>\r
+<eng-data cg="48.5" f="349." m="17.5184" t="0.2"/>\r
+<eng-data cg="48.5" f="310." m="10.3161" t="0.25"/>\r
+<eng-data cg="48.5" f="264." m="4.04271" t="0.3"/>\r
+<eng-data cg="48.5" f="257." m="1.30954" t="0.324"/>\r
+<eng-data cg="48.5" f="39." m="0.144921" t="0.342"/>\r
+<eng-data cg="48.5" f="0." m="0." t="0.359"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-G35EJ 29 98 4-7 0.05 0.1005 AeroTech\r
-0.01 39.14\r
-0.02 76.22\r
-0.05 64.46\r
-0.13 57.54\r
-0.21 57.53\r
-0.24 64.43\r
-0.25 57.06\r
-0.35 56.12\r
-0.43 55.2\r
-0.48 57.49\r
-0.51 52.41\r
-0.55 53.33\r
-0.76 50.54\r
-0.91 50.06\r
-1.11 44.96\r
-1.32 41.24\r
-1.55 35.68\r
-1.6 36.13\r
-1.63 33.36\r
-1.67 34.28\r
-1.8 30.12\r
-2 25.02\r
-2.14 21.32\r
-2.23 19.46\r
-2.3 15.77\r
-2.41 9.76\r
-2.53 6.52\r
-2.65 3.74\r
-2.74 1.88\r
-2.91 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="205.89" Itot="100.956" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="34.693" burn-time="2.91" cgDiv="10" cgFix="1" cgStep="-1." code="G35EJ" delays="4,7" dia="29." exitDia="0." initWt="100.5" len="98." mDiv="10" mFix="1" mStep="-1." massFrac="49.75" mfg="Aerotech" peakThrust="76.22" propWt="50." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="49." f="0." m="50." t="0."/>\r
+<eng-data cg="49." f="39.14" m="49.9031" t="0.01"/>\r
+<eng-data cg="49." f="76.22" m="49.6174" t="0.02"/>\r
+<eng-data cg="49." f="64.46" m="48.5723" t="0.05"/>\r
+<eng-data cg="49." f="57.54" m="46.1554" t="0.13"/>\r
+<eng-data cg="49." f="57.53" m="43.8758" t="0.21"/>\r
+<eng-data cg="49." f="64.43" m="42.9698" t="0.24"/>\r
+<eng-data cg="49." f="57.06" m="42.6689" t="0.25"/>\r
+<eng-data cg="49." f="56.12" m="39.8662" t="0.35"/>\r
+<eng-data cg="49." f="55.2" m="37.6609" t="0.43"/>\r
+<eng-data cg="49." f="57.49" m="36.2657" t="0.48"/>\r
+<eng-data cg="49." f="52.41" m="35.4492" t="0.51"/>\r
+<eng-data cg="49." f="53.33" m="34.4018" t="0.55"/>\r
+<eng-data cg="49." f="50.54" m="29.0003" t="0.76"/>\r
+<eng-data cg="49." f="50.06" m="25.2636" t="0.91"/>\r
+<eng-data cg="49." f="44.96" m="20.5576" t="1.11"/>\r
+<eng-data cg="49." f="41.24" m="16.075" t="1.32"/>\r
+<eng-data cg="49." f="35.68" m="11.694" t="1.55"/>\r
+<eng-data cg="49." f="36.13" m="10.8048" t="1.6"/>\r
+<eng-data cg="49." f="33.36" m="10.2886" t="1.63"/>\r
+<eng-data cg="49." f="34.28" m="9.6186" t="1.67"/>\r
+<eng-data cg="49." f="30.12" m="7.54543" t="1.8"/>\r
+<eng-data cg="49." f="25.02" m="4.81455" t="2."/>\r
+<eng-data cg="49." f="21.32" m="3.20802" t="2.14"/>\r
+<eng-data cg="49." f="19.46" m="2.29916" t="2.23"/>\r
+<eng-data cg="49." f="15.77" m="1.68848" t="2.3"/>\r
+<eng-data cg="49." f="9.76" m="0.993052" t="2.41"/>\r
+<eng-data cg="49." f="6.52" m="0.509279" t="2.53"/>\r
+<eng-data cg="49." f="3.74" m="0.204395" t="2.65"/>\r
+<eng-data cg="49." f="1.88" m="0.079143" t="2.74"/>\r
+<eng-data cg="49." f="0." m="0." t="2.91"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech G38FJ RASP.ENG file made by Tim Van Milligan\r
-;For RockSim www.RockSim.com\r
-;File Created March 2, 2005\r
-;Thrust curve supplied by Aerotech for the molded case G38FJ motors.\r
-G38FJ 29 124 4-7 0.0597 0.1264 Aerotech\r
-0.024 52.928\r
-0.171 48.424\r
-0.497 45.045\r
-1 42.23\r
-1.279 39.978\r
-1.498 36.599\r
-1.783 30.406\r
-2.011 23.086\r
-2.272 10.135\r
-2.467 3.941\r
-2.64 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="148.29" Itot="86.818" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="32.886" burn-time="2.64" cgDiv="10" cgFix="1" cgStep="-1." code="G38FJ" delays="4,7" dia="29." exitDia="0." initWt="126.4" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="47.23" mfg="Aerotech" peakThrust="52.928" propWt="59.7" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech G38FJ RASP.ENG file made by Tim Van Milligan\r
+For RockSim www.RockSim.com\r
+File Created March 2, 2005\r
+Thrust curve supplied by Aerotech for the molded case G38FJ motors.\r
+</comments>\r
+<data>\r
+<eng-data cg="62." f="0." m="59.7" t="0."/>\r
+<eng-data cg="62." f="52.928" m="59.2633" t="0.024"/>\r
+<eng-data cg="62." f="48.424" m="54.1407" t="0.171"/>\r
+<eng-data cg="62." f="45.045" m="43.6641" t="0.497"/>\r
+<eng-data cg="62." f="42.23" m="28.5705" t="1."/>\r
+<eng-data cg="62." f="39.978" m="20.6845" t="1.279"/>\r
+<eng-data cg="62." f="36.599" m="14.9185" t="1.498"/>\r
+<eng-data cg="62." f="30.406" m="8.35267" t="1.783"/>\r
+<eng-data cg="62." f="23.086" m="4.15934" t="2.011"/>\r
+<eng-data cg="62." f="10.135" m="1.17815" t="2.272"/>\r
+<eng-data cg="62." f="3.941" m="0.234417" t="2.467"/>\r
+<eng-data cg="62." f="0." m="0." t="2.64"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech G40W RASP.ENG file made by Tim Van Milligan\r
-;For RockSim www.RockSim.com\r
-;File Created March 2, 2005\r
-;Thrust curve supplied by Aerotech for the molded case G40W motors.\r
-G40W 29 124 4-7-10 0.0538 0.123 AeroTech\r
-0.024 74.325\r
-0.057 67.005\r
-0.252 65.879\r
-0.5 63.063\r
-0.765 60.248\r
-1 54.054\r
-1.25 47.298\r
-1.502 36.599\r
-1.751 25.338\r
-1.999 12.951\r
-2.121 3.941\r
-2.3 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="187.68" Itot="99.02" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="43.052" burn-time="2.3" cgDiv="10" cgFix="1" cgStep="-1." code="G40W" delays="4,7,10" dia="29." exitDia="0." initWt="123." len="124." mDiv="10" mFix="1" mStep="-1." massFrac="43.74" mfg="Aerotech" peakThrust="74.325" propWt="53.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech G40W RASP.ENG file made by Tim Van Milligan\r
+For RockSim www.RockSim.com\r
+File Created March 2, 2005\r
+Thrust curve supplied by Aerotech for the molded case G40W motors.\r
+</comments>\r
+<data>\r
+<eng-data cg="62." f="0." m="53.8" t="0."/>\r
+<eng-data cg="62." f="74.325" m="53.3154" t="0.024"/>\r
+<eng-data cg="62." f="67.005" m="52.0484" t="0.057"/>\r
+<eng-data cg="62." f="65.879" m="45.009" t="0.252"/>\r
+<eng-data cg="62." f="63.063" m="36.3219" t="0.5"/>\r
+<eng-data cg="62." f="60.248" m="27.4447" t="0.765"/>\r
+<eng-data cg="62." f="54.054" m="20.1476" t="1."/>\r
+<eng-data cg="62." f="47.298" m="13.2642" t="1.25"/>\r
+<eng-data cg="62." f="36.599" m="7.52075" t="1.502"/>\r
+<eng-data cg="62." f="25.338" m="3.3311" t="1.751"/>\r
+<eng-data cg="62." f="12.951" m="0.751488" t="1.999"/>\r
+<eng-data cg="62." f="3.941" m="0.191641" t="2.121"/>\r
+<eng-data cg="62." f="0." m="0." t="2.3"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; G53FJ based on Aerotech instruction sheet by C. Kobel 12/9/07\r
-G53FJ 29 124 5-7-10 0.060 0.152 AT\r
- 0.012 44.898\r
- 0.031 71.504\r
- 0.064 80.234\r
- 0.081 83.976\r
- 0.100 86.47\r
- 0.150 84.599\r
- 0.200 81.897\r
- 0.300 78.571\r
- 0.400 76.493\r
- 0.500 73.583\r
- 0.600 70.881\r
- 0.700 67.347\r
- 0.800 63.813\r
- 0.900 60.072\r
- 1.000 54.667\r
- 1.100 47.392\r
- 1.200 39.909\r
- 1.300 32.426\r
- 1.400 25.983\r
- 1.500 20.578\r
- 1.600 10.601\r
- 1.700 3.949\r
- 1.800 1.247\r
- 1.850 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Aerotech" code="G53FJ" Type="reloadable" dia="29." len="124." initWt="147."\r
+propWt="60." delays="5,7,10" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="45.499" peakThrust="85.647" throatDia="0." exitDia="0." Itot="90.993"\r
+burn-time="2." massFrac="40.82" Isp="154.65" tDiv="10" tStep="-1." tFix="1"\r
+FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+ <comments>@File: G53FJ_Combined.txt, @Pts-I: 1310, @Pts-O: 32, @Sm: 2, @CO: 5%\r
+@TI: 90.9683, @TIa: 90.6677, @TIe: 0.0%, @ThMax: 85.8995, @ThAvg: 52.9292, @Tb: 1.713\r
+Exported using ThrustCurveTool, www.ThrustGear.com\r
+</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="60." cg="62."/>\r
+ <eng-data t="0." f="0.0161325" m="60." cg="62."/>\r
+ <eng-data t="0.084" f="0.173372" m="59.9948" cg="62."/>\r
+ <eng-data t="0.098" f="0.875543" m="59.9899" cg="62."/>\r
+ <eng-data t="0.102" f="1.97607" m="59.9861" cg="62."/>\r
+ <eng-data t="0.104" f="3.2865" m="59.9827" cg="62."/>\r
+ <eng-data t="0.106" f="5.66335" m="59.9768" cg="62."/>\r
+ <eng-data t="0.108" f="10.0044" m="59.9664" cg="62."/>\r
+ <eng-data t="0.112" f="26.8138" m="59.9179" cg="62."/>\r
+ <eng-data t="0.114" f="36.5078" m="59.8761" cg="62."/>\r
+ <eng-data t="0.118" f="51.1937" m="59.7605" cg="62."/>\r
+ <eng-data t="0.12" f="56.7099" m="59.6893" cg="62."/>\r
+ <eng-data t="0.124" f="64.8595" m="59.529" cg="62."/>\r
+ <eng-data t="0.128" f="70.2176" m="59.3509" cg="62."/>\r
+ <eng-data t="0.134" f="74.2385" m="59.0651" cg="62."/>\r
+ <eng-data t="0.146" f="78.8965" m="58.4593" cg="62."/>\r
+ <eng-data t="0.152" f="79.8043" m="58.1453" cg="62."/>\r
+ <eng-data t="0.164" f="83.1003" m="57.5008" cg="62."/>\r
+ <eng-data t="0.188" f="85.6475" m="56.1656" cg="62."/>\r
+ <eng-data t="0.234" f="85.447" m="53.5708" cg="62."/>\r
+ <eng-data t="0.298" f="82.0177" m="50.0372" cg="62."/>\r
+ <eng-data t="0.354" f="79.7728" m="47.0501" cg="62."/>\r
+ <eng-data t="0.748" f="69.4245" m="27.6694" cg="62."/>\r
+ <eng-data t="1.0239" f="56.7367" m="16.1934" cg="62."/>\r
+ <eng-data t="1.1599" f="48.3545" m="11.4813" cg="62."/>\r
+ <eng-data t="1.3439" f="35.2918" m="6.40698" cg="62."/>\r
+ <eng-data t="1.5599" f="22.1026" m="2.31969" cg="62."/>\r
+ <eng-data t="1.5999" f="19.2471" m="1.77438" cg="62."/>\r
+ <eng-data t="1.6979" f="11.0049" m="0.796939" cg="62."/>\r
+ <eng-data t="1.7699" f="6.58917" m="0.379291" cg="62."/>\r
+ <eng-data t="1.8179" f="4.26533" m="0.207515" cg="62."/>\r
+ <eng-data t="1.9179" f="1.11474" m="0.030137" cg="62."/>\r
+ <eng-data t="1.9999" f="0." m="0." cg="62."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech G54 RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-G54 29 124 6-10-14 0.046 0.1365 AT\r
-0.018 10.953\r
-0.042 39.215\r
-0.083 66.888\r
-0.14 72.075\r
-0.223 74.958\r
-0.25 76.694\r
-0.282 80.156\r
-0.315 79.577\r
-0.336 79.577\r
-0.354 81.64\r
-0.365 77.841\r
-0.374 80.724\r
-0.389 76.694\r
-0.455 76.116\r
-0.523 74.39\r
-0.639 70.928\r
-0.722 67.467\r
-0.82 64.005\r
-0.897 58.817\r
-0.992 51.894\r
-1.084 43.824\r
-1.197 34.017\r
-1.268 28.251\r
-1.283 29.987\r
-1.295 27.104\r
-1.328 23.642\r
-1.366 16.719\r
-1.399 9.803\r
-1.435 4.612\r
-1.51 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="179.67" Itot="81.05" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="53.676" burn-time="1.51" cgDiv="10" cgFix="1" cgStep="-1." code="G54" delays="6,10,14" dia="29." exitDia="0." initWt="136.5" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="33.7" mfg="Aerotech" peakThrust="81.64" propWt="46." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech G54 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="62." f="0." m="46." t="0."/>\r
+<eng-data cg="62." f="10.953" m="45.9441" t="0.018"/>\r
+<eng-data cg="62." f="39.215" m="45.6024" t="0.042"/>\r
+<eng-data cg="62." f="66.888" m="44.3679" t="0.083"/>\r
+<eng-data cg="62." f="72.075" m="42.1202" t="0.14"/>\r
+<eng-data cg="62." f="74.958" m="38.657" t="0.223"/>\r
+<eng-data cg="62." f="76.694" m="37.4951" t="0.25"/>\r
+<eng-data cg="62." f="80.156" m="36.0708" t="0.282"/>\r
+<eng-data cg="62." f="79.577" m="34.575" t="0.315"/>\r
+<eng-data cg="62." f="79.577" m="33.6265" t="0.336"/>\r
+<eng-data cg="62." f="81.64" m="32.803" t="0.354"/>\r
+<eng-data cg="62." f="77.841" m="32.3052" t="0.365"/>\r
+<eng-data cg="62." f="80.724" m="31.9002" t="0.374"/>\r
+<eng-data cg="62." f="76.694" m="31.2302" t="0.389"/>\r
+<eng-data cg="62." f="76.116" m="28.3682" t="0.455"/>\r
+<eng-data cg="62." f="74.39" m="25.4639" t="0.523"/>\r
+<eng-data cg="62." f="70.928" m="20.6804" t="0.639"/>\r
+<eng-data cg="62." f="67.467" m="17.4207" t="0.722"/>\r
+<eng-data cg="62." f="64.005" m="13.7645" t="0.82"/>\r
+<eng-data cg="62." f="58.817" m="11.0807" t="0.897"/>\r
+<eng-data cg="62." f="51.894" m="8.09613" t="0.992"/>\r
+<eng-data cg="62." f="43.824" m="5.5972" t="1.084"/>\r
+<eng-data cg="62." f="34.017" m="3.10111" t="1.197"/>\r
+<eng-data cg="62." f="28.251" m="1.84654" t="1.268"/>\r
+<eng-data cg="62." f="29.987" m="1.59864" t="1.283"/>\r
+<eng-data cg="62." f="27.104" m="1.40423" t="1.295"/>\r
+<eng-data cg="62." f="23.642" m="0.929016" t="1.328"/>\r
+<eng-data cg="62." f="16.719" m="0.493786" t="1.366"/>\r
+<eng-data cg="62." f="9.803" m="0.245419" t="1.399"/>\r
+<eng-data cg="62." f="4.612" m="0.0981575" t="1.435"/>\r
+<eng-data cg="62." f="0." m="0." t="1.51"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech G55 RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-G55 24 117 5-10-15 0.0625 0.1148 AeroTech\r
-0.009 81.136\r
-0.014 84.65\r
-0.034 80.557\r
-0.084 77.064\r
-0.13 71.823\r
-0.18 72.422\r
-0.206 68.919\r
-0.342 69.538\r
-0.483 68.989\r
-0.513 66.663\r
-0.543 68.42\r
-0.664 66.114\r
-0.876 66.164\r
-0.901 64.418\r
-0.997 65.026\r
-1.062 66.793\r
-1.088 63.879\r
-1.148 63.889\r
-1.158 66.813\r
-1.173 63.31\r
-1.209 62.741\r
-1.325 61.593\r
-1.395 59.277\r
-1.456 57.541\r
-1.486 58.129\r
-1.587 52.32\r
-1.708 40.094\r
-1.824 26.11\r
-1.95 15.63\r
-2.112 7.498\r
-2.258 3.446\r
-2.44 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="195.08" Itot="119.567" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="49.003" burn-time="2.44" cgDiv="10" cgFix="1" cgStep="-1." code="G55" delays="5,10,15" dia="24." exitDia="0." initWt="114.8" len="117." mDiv="10" mFix="1" mStep="-1." massFrac="54.44" mfg="Aerotech" peakThrust="84.65" propWt="62.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech G55 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="58.5" f="0." m="62.5" t="0."/>\r
+<eng-data cg="58.5" f="81.136" m="62.3091" t="0.009"/>\r
+<eng-data cg="58.5" f="84.65" m="62.0925" t="0.014"/>\r
+<eng-data cg="58.5" f="80.557" m="61.2289" t="0.034"/>\r
+<eng-data cg="58.5" f="77.064" m="59.1691" t="0.084"/>\r
+<eng-data cg="58.5" f="71.823" m="57.3791" t="0.13"/>\r
+<eng-data cg="58.5" f="72.422" m="55.4941" t="0.18"/>\r
+<eng-data cg="58.5" f="68.919" m="54.5337" t="0.206"/>\r
+<eng-data cg="58.5" f="69.538" m="49.6122" t="0.342"/>\r
+<eng-data cg="58.5" f="68.989" m="44.5073" t="0.483"/>\r
+<eng-data cg="58.5" f="66.663" m="43.4436" t="0.513"/>\r
+<eng-data cg="58.5" f="68.42" m="42.3845" t="0.543"/>\r
+<eng-data cg="58.5" f="66.114" m="38.1299" t="0.664"/>\r
+<eng-data cg="58.5" f="66.164" m="30.8006" t="0.876"/>\r
+<eng-data cg="58.5" f="64.418" m="29.9474" t="0.901"/>\r
+<eng-data cg="58.5" f="65.026" m="26.6996" t="0.997"/>\r
+<eng-data cg="58.5" f="66.793" m="24.4602" t="1.062"/>\r
+<eng-data cg="58.5" f="63.879" m="23.5722" t="1.088"/>\r
+<eng-data cg="58.5" f="63.889" m="21.5686" t="1.148"/>\r
+<eng-data cg="58.5" f="66.813" m="21.227" t="1.158"/>\r
+<eng-data cg="58.5" f="63.31" m="20.7169" t="1.173"/>\r
+<eng-data cg="58.5" f="62.741" m="19.5308" t="1.209"/>\r
+<eng-data cg="58.5" f="61.593" m="15.7613" t="1.325"/>\r
+<eng-data cg="58.5" f="59.277" m="13.55" t="1.395"/>\r
+<eng-data cg="58.5" f="57.541" m="11.6875" t="1.456"/>\r
+<eng-data cg="58.5" f="58.129" m="10.7806" t="1.486"/>\r
+<eng-data cg="58.5" f="52.32" m="7.86504" t="1.587"/>\r
+<eng-data cg="58.5" f="40.094" m="4.94249" t="1.708"/>\r
+<eng-data cg="58.5" f="26.11" m="2.93533" t="1.824"/>\r
+<eng-data cg="58.5" f="15.63" m="1.56077" t="1.95"/>\r
+<eng-data cg="58.5" f="7.498" m="0.581525" t="2.112"/>\r
+<eng-data cg="58.5" f="3.446" m="0.163918" t="2.258"/>\r
+<eng-data cg="58.5" f="0." m="0." t="2.44"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;G61W Data Entered by Tim Van Milligan\r
-;For RockSim: www.RockSim.com\r
-;Based on TRA Certification Test date: June 13, 2004\r
-;Not Approved by TRA or Aerotech\r
-G61W 38 106.7 6-10-14 0.0613 0.1904 AT\r
-0.008 3.083\r
-0.054 71.348\r
-0.089 72.229\r
-0.174 75.312\r
-0.216 78.394\r
-0.247 79.716\r
-0.502 81.037\r
-0.753 77.073\r
-1.001 72.669\r
-1.132 66.944\r
-1.252 55.933\r
-1.503 38.316\r
-1.754 10.13\r
-1.905 3.523\r
-2.04 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="184.29" Itot="110.787" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="54.307" burn-time="2.04" cgDiv="10" cgFix="1" cgStep="-1." code="G61W" delays="6,10,14" dia="38." exitDia="0." initWt="190.4" len="106.7" mDiv="10" mFix="1" mStep="-1." massFrac="32.2" mfg="Aerotech" peakThrust="81.037" propWt="61.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>G61W Data Entered by Tim Van Milligan\r
+For RockSim: www.RockSim.com\r
+Based on TRA Certification Test date: June 13, 2004\r
+Not Approved by TRA or Aerotech\r
+</comments>\r
+<data>\r
+<eng-data cg="53.35" f="0." m="61.3" t="0."/>\r
+<eng-data cg="53.35" f="3.083" m="61.2932" t="0.008"/>\r
+<eng-data cg="53.35" f="71.348" m="60.3459" t="0.054"/>\r
+<eng-data cg="53.35" f="72.229" m="58.9557" t="0.089"/>\r
+<eng-data cg="53.35" f="75.312" m="55.4861" t="0.174"/>\r
+<eng-data cg="53.35" f="78.394" m="53.7001" t="0.216"/>\r
+<eng-data cg="53.35" f="79.716" m="52.3441" t="0.247"/>\r
+<eng-data cg="53.35" f="81.037" m="41.0034" t="0.502"/>\r
+<eng-data cg="53.35" f="77.073" m="30.024" t="0.753"/>\r
+<eng-data cg="53.35" f="72.669" m="19.7501" t="1.001"/>\r
+<eng-data cg="53.35" f="66.944" m="14.6902" t="1.132"/>\r
+<eng-data cg="53.35" f="55.933" m="10.6108" t="1.252"/>\r
+<eng-data cg="53.35" f="38.316" m="4.06608" t="1.503"/>\r
+<eng-data cg="53.35" f="10.13" m="0.701938" t="1.754"/>\r
+<eng-data cg="53.35" f="3.523" m="0.13158" t="1.905"/>\r
+<eng-data cg="53.35" f="0." m="0." t="2.04"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech G64 RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-G64 29 124 4-8-10 0.0625 0.1512 AT\r
-0.014 54.325\r
-0.032 81.488\r
-0.059 98.31\r
-0.101 85.021\r
-0.165 83.847\r
-0.274 85.614\r
-0.37 87.39\r
-0.476 86.798\r
-0.503 91.516\r
-0.517 85.614\r
-0.585 83.847\r
-0.723 80.896\r
-0.745 82.07\r
-0.773 77.945\r
-0.883 75.576\r
-0.988 74.401\r
-1.093 69.673\r
-1.262 61.412\r
-1.28 61.994\r
-1.326 58.451\r
-1.372 54.907\r
-1.422 47.238\r
-1.505 34.841\r
-1.591 23.027\r
-1.701 13.581\r
-1.829 7.085\r
-1.902 4.133\r
-1.966 1.771\r
-2.09 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="193.83" Itot="118.803" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="56.844" burn-time="2.09" cgDiv="10" cgFix="1" cgStep="-1." code="G64" delays="4,8,10" dia="29." exitDia="0." initWt="151.2" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="41.34" mfg="Aerotech" peakThrust="98.31" propWt="62.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech G64 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="62." f="0." m="62.5" t="0."/>\r
+<eng-data cg="62." f="54.325" m="62.2999" t="0.014"/>\r
+<eng-data cg="62." f="81.488" m="61.6569" t="0.032"/>\r
+<eng-data cg="62." f="98.31" m="60.38" t="0.059"/>\r
+<eng-data cg="62." f="85.021" m="58.3546" t="0.101"/>\r
+<eng-data cg="62." f="83.847" m="55.5117" t="0.165"/>\r
+<eng-data cg="62." f="85.614" m="50.6531" t="0.274"/>\r
+<eng-data cg="62." f="87.39" m="46.2844" t="0.37"/>\r
+<eng-data cg="62." f="86.798" m="41.4276" t="0.476"/>\r
+<eng-data cg="62." f="91.516" m="40.1612" t="0.503"/>\r
+<eng-data cg="62." f="85.614" m="39.5089" t="0.517"/>\r
+<eng-data cg="62." f="83.847" m="36.4778" t="0.585"/>\r
+<eng-data cg="62." f="80.896" m="30.4977" t="0.723"/>\r
+<eng-data cg="62." f="82.07" m="29.5546" t="0.745"/>\r
+<eng-data cg="62." f="77.945" m="28.3761" t="0.773"/>\r
+<eng-data cg="62." f="75.576" m="23.9341" t="0.883"/>\r
+<eng-data cg="62." f="74.401" m="19.7918" t="0.988"/>\r
+<eng-data cg="62." f="69.673" m="15.8126" t="1.093"/>\r
+<eng-data cg="62." f="61.412" m="9.98534" t="1.262"/>\r
+<eng-data cg="62." f="61.994" m="9.40105" t="1.28"/>\r
+<eng-data cg="62." f="58.451" m="7.94368" t="1.326"/>\r
+<eng-data cg="62." f="54.907" m="6.57206" t="1.372"/>\r
+<eng-data cg="62." f="47.238" m="5.22865" t="1.422"/>\r
+<eng-data cg="62." f="34.841" m="3.43667" t="1.505"/>\r
+<eng-data cg="62." f="23.027" m="2.12761" t="1.591"/>\r
+<eng-data cg="62." f="13.581" m="1.06837" t="1.701"/>\r
+<eng-data cg="62." f="7.085" m="0.372564" t="1.829"/>\r
+<eng-data cg="62." f="4.133" m="0.157156" t="1.902"/>\r
+<eng-data cg="62." f="1.771" m="0.0577648" t="1.966"/>\r
+<eng-data cg="62." f="0." m="0." t="2.09"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; Aerotech G67R (Redline)\r
-;\r
-; AeroTech RMS-38/120 EZ Access Reloadable Motors (New! Hardware).\r
-; New AeroTech Redline Motor. Just announced on AeroTech's Website!\r
-; File produced 28 Feb 2005.\r
-;\r
-; The file was produced by scaling data points off the\r
-; thrust curve in the manufacturers catalog sheet.\r
-;\r
-; The motor is not yet on www.thrustcurve.org.\r
-; Hence the amateur file production.\r
-; The file was created by Stan Hemphill.\r
-; Contact at stanley_hemphill@hotmail.com.\r
-;\r
-; Motor Dia Len Delay Prop Gross Mfg\r
-G67R 38 106 4-6-8-9-10-12-13-15-17 0.0576 0.191 AT\r
-0.0400 004.9200\r
-0.0500 006.5600\r
-0.0600 009.8400\r
-0.0700 016.4100\r
-0.0800 032.8100\r
-0.1000 049.2200\r
-0.1300 068.0800\r
-0.1500 076.2900\r
-0.1800 080.3900\r
-0.2400 082.8500\r
-0.2600 085.3100\r
-0.3100 087.7700\r
-0.5100 089.4100\r
-0.5300 091.0500\r
-0.5600 087.7700\r
-0.6000 086.9500\r
-0.6100 088.5900\r
-0.6700 086.9500\r
-0.6900 085.3100\r
-0.7100 086.9500\r
-0.7200 085.3100\r
-0.7400 086.1300\r
-0.7700 085.3100\r
-0.8100 082.0300\r
-0.9500 078.7500\r
-1.0500 073.8200\r
-1.4300 053.3200\r
-1.5000 052.5000\r
-1.5200 050.8600\r
-1.5400 045.9400\r
-1.6200 011.4800\r
-1.6400 000.0000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="193.91" Itot="109.53" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="68.456" burn-time="1.6" cgDiv="10" cgFix="1" cgStep="-1." code="G67R" delays="10" dia="38." exitDia="0." initWt="191." len="106.43" mDiv="10" mFix="1" mStep="-1." massFrac="30.16" mfg="Aerotech" peakThrust="90.425" propWt="57.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>G67R Data Entered by Tim Van Milligan\r
+For RockSim: www.RockSim.com\r
+Based on Aerotech's Reload Kit Instruction Sheet.\r
+Not Officially Approved by TRA or Aerotech\r
+</comments>\r
+<data>\r
+<eng-data cg="53.215" f="0." m="57.6" t="0."/>\r
+<eng-data cg="53.215" f="11.795" m="57.4728" t="0.041"/>\r
+<eng-data cg="53.215" f="57.288" m="56.4375" t="0.098"/>\r
+<eng-data cg="53.215" f="71.329" m="55.7273" t="0.119"/>\r
+<eng-data cg="53.215" f="75.822" m="54.5278" t="0.15"/>\r
+<eng-data cg="53.215" f="80.877" m="52.4677" t="0.2"/>\r
+<eng-data cg="53.215" f="88.74" m="48.0077" t="0.3"/>\r
+<eng-data cg="53.215" f="89.301" m="43.3263" t="0.4"/>\r
+<eng-data cg="53.215" f="90.425" m="38.7423" t="0.497"/>\r
+<eng-data cg="53.215" f="89.301" m="33.5913" t="0.606"/>\r
+<eng-data cg="53.215" f="85.932" m="25.0672" t="0.791"/>\r
+<eng-data cg="53.215" f="75.26" m="16.0818" t="1.003"/>\r
+<eng-data cg="53.215" f="64.589" m="9.20544" t="1.19"/>\r
+<eng-data cg="53.215" f="58.411" m="5.68019" t="1.299"/>\r
+<eng-data cg="53.215" f="55.041" m="2.69707" t="1.399"/>\r
+<eng-data cg="53.215" f="52.233" m="2.02011" t="1.423"/>\r
+<eng-data cg="53.215" f="47.74" m="1.15264" t="1.456"/>\r
+<eng-data cg="53.215" f="22.466" m="0.395774" t="1.497"/>\r
+<eng-data cg="53.215" f="12.356" m="0.203495" t="1.518"/>\r
+<eng-data cg="53.215" f="2.808" m="0.0280569" t="1.562"/>\r
+<eng-data cg="53.215" f="0." m="0." t="1.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Submitted to ThrustCurve.org by Chris Kobel (4/13/07)\r
-; G69N based on Aerotech instruction sheet by C. Kobel 3/29/07\r
-G69N 38 106 0 0.0622 0.195 AT\r
- 0.020 51.972\r
- 0.050 75.574\r
- 0.100 76.709\r
- 0.200 77.617\r
- 0.300 79.206\r
- 0.400 81.475\r
- 0.500 84.425\r
- 0.600 86.922\r
- 0.700 88.737\r
- 0.800 89.645\r
- 0.900 91.688\r
- 1.000 93.503\r
- 1.100 94.411\r
- 1.200 94.638\r
- 1.300 93.957\r
- 1.350 93.05\r
- 1.400 89.418\r
- 1.500 62.865\r
- 1.600 33.362\r
- 1.650 19.518\r
- 1.700 12.028\r
- 1.750 7.489\r
- 1.800 4.539\r
- 1.900 1.816\r
- 2.000 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="223.45" Itot="136.301" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="68.151" burn-time="2." cgDiv="10" cgFix="1" cgStep="-1." code="G69N" delays="1000" dia="38." exitDia="0." initWt="201." len="106." mDiv="10" mFix="1" mStep="-1." massFrac="30.95" mfg="Aerotech" peakThrust="86.441" propWt="62.2" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>NAR Test Data\r
+March 23, 2007\r
+</comments>\r
+<data>\r
+<eng-data cg="53." f="0." m="62.2" t="0."/>\r
+<eng-data cg="53." f="0.05" m="62.2" t="0.001"/>\r
+<eng-data cg="53." f="1.04339" m="62.1997" t="0.002"/>\r
+<eng-data cg="53." f="1.49626" m="62.1974" t="0.006"/>\r
+<eng-data cg="53." f="3.99151" m="62.1924" t="0.01"/>\r
+<eng-data cg="53." f="7.18827" m="62.1873" t="0.012"/>\r
+<eng-data cg="53." f="31.7855" m="62.1517" t="0.016"/>\r
+<eng-data cg="53." f="38.6675" m="62.1196" t="0.018"/>\r
+<eng-data cg="53." f="43.507" m="62.0821" t="0.02"/>\r
+<eng-data cg="53." f="55.3616" m="61.9016" t="0.028"/>\r
+<eng-data cg="53." f="58.4696" m="61.7458" t="0.034"/>\r
+<eng-data cg="53." f="63.3535" m="61.579" t="0.04"/>\r
+<eng-data cg="53." f="66.4615" m="61.5198" t="0.042"/>\r
+<eng-data cg="53." f="74.0094" m="61.1351" t="0.054"/>\r
+<eng-data cg="53." f="76.2294" m="60.7238" t="0.066"/>\r
+<eng-data cg="53." f="75.7854" m="58.712" t="0.124"/>\r
+<eng-data cg="53." f="77.5614" m="57.1025" t="0.17"/>\r
+<eng-data cg="53." f="82.0013" m="38.9716" t="0.668"/>\r
+<eng-data cg="53." f="83.7773" m="37.0046" t="0.72"/>\r
+<eng-data cg="53." f="86.4412" m="21.3176" t="1.1239"/>\r
+<eng-data cg="53." f="85.9972" m="9.82874" t="1.4159"/>\r
+<eng-data cg="53." f="84.2213" m="8.04215" t="1.4619"/>\r
+<eng-data cg="53." f="80.2253" m="6.76641" t="1.4959"/>\r
+<eng-data cg="53." f="71.7894" m="5.10151" t="1.5439"/>\r
+<eng-data cg="53." f="29.832" m="1.34521" t="1.7059"/>\r
+<eng-data cg="53." f="20.7301" m="0.860669" t="1.7479"/>\r
+<eng-data cg="53." f="9.23064" m="0.327448" t="1.8259"/>\r
+<eng-data cg="53." f="4.21351" m="0.0943133" t="1.9019"/>\r
+<eng-data cg="53." f="0." m="0." t="2."/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; G71R based on Aerotech instruction sheet by C. Kobel 3/29/07\r
-G71R 29 124 4-7-10 0.0569 0.147 AT\r
- 0.000 0.389\r
- 0.050 109.714\r
- 0.100 117.884\r
- 0.200 113.216\r
- 0.300 109.714\r
- 0.400 105.045\r
- 0.500 99.21\r
- 0.600 92.207\r
- 0.700 83.258\r
- 0.800 75.477\r
- 0.900 68.085\r
- 1.000 57.97\r
- 1.100 47.465\r
- 1.200 33.848\r
- 1.300 21.009\r
- 1.400 11.283\r
- 1.500 5.447\r
- 1.600 2.334\r
- 1.700 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="191.57" Itot="106.894" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="62.879" burn-time="1.7" cgDiv="10" cgFix="1" cgStep="-1." code="G71R" delays="4,7,10" dia="29." exitDia="0." initWt="147." len="124." mDiv="10" mFix="1" mStep="-1." massFrac="38.71" mfg="Aerotech" peakThrust="117.884" propWt="56.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>G71R based on Aerotech instruction sheet by C. Kobel 3/29/07</comments>\r
+<data>\r
+<eng-data cg="62." f="0." m="56.9" t="0."/>\r
+<eng-data cg="62." f="0.389" m="56.9" t="0."/>\r
+<eng-data cg="62." f="109.714" m="55.4348" t="0.05"/>\r
+<eng-data cg="62." f="117.884" m="52.406" t="0.1"/>\r
+<eng-data cg="62." f="113.216" m="46.2552" t="0.2"/>\r
+<eng-data cg="62." f="109.714" m="40.3219" t="0.3"/>\r
+<eng-data cg="62." f="105.045" m="34.606" t="0.4"/>\r
+<eng-data cg="62." f="99.21" m="29.1697" t="0.5"/>\r
+<eng-data cg="62." f="92.207" m="24.0751" t="0.6"/>\r
+<eng-data cg="62." f="83.258" m="19.405" t="0.7"/>\r
+<eng-data cg="62." f="75.477" m="15.1803" t="0.8"/>\r
+<eng-data cg="62." f="68.085" m="11.3593" t="0.9"/>\r
+<eng-data cg="62." f="57.97" m="8.00433" t="1."/>\r
+<eng-data cg="62." f="47.465" m="5.19815" t="1.1"/>\r
+<eng-data cg="62." f="33.848" m="3.03398" t="1.2"/>\r
+<eng-data cg="62." f="21.009" m="1.57395" t="1.3"/>\r
+<eng-data cg="62." f="11.283" m="0.714487" t="1.4"/>\r
+<eng-data cg="62." f="5.447" m="0.269213" t="1.5"/>\r
+<eng-data cg="62." f="2.334" m="0.06212" t="1.6"/>\r
+<eng-data cg="62." f="0." m="0." t="1.7"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech G75J\r
-; Copyright Tripoli Motor Testing 1997 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-G75J 29 194 10 0.112 0.23296 AT\r
- 0.047 65.701\r
- 0.143 68.564\r
- 0.239 72.143\r
- 0.334 73.261\r
- 0.430 73.960\r
- 0.526 75.036\r
- 0.622 75.705\r
- 0.718 75.030\r
- 0.814 77.886\r
- 0.909 76.183\r
- 1.005 76.852\r
- 1.101 75.729\r
- 1.197 78.854\r
- 1.293 78.669\r
- 1.389 76.464\r
- 1.484 76.440\r
- 1.580 74.976\r
- 1.676 72.657\r
- 1.772 69.460\r
- 1.868 62.121\r
- 1.964 39.090\r
- 2.059 19.703\r
- 2.155 7.554\r
- 2.251 2.062\r
- 2.347 0.382\r
- 2.443 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="155.88" Itot="161.429" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="73.377" burn-time="2.2" cgDiv="10" cgFix="1" cgStep="-1." code="G75J" delays="6,10" dia="29." exitDia="0." initWt="227.9" len="195." mDiv="10" mFix="1" mStep="-1." massFrac="46.34" mfg="Aerotech" peakThrust="87.27" propWt="105.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="97.5" f="0." m="105.6" t="0."/>\r
+<eng-data cg="97.5" f="0.04" m="105.6" t="0."/>\r
+<eng-data cg="97.5" f="82.64" m="102.896" t="0.1"/>\r
+<eng-data cg="97.5" f="78.06" m="97.6396" t="0.2"/>\r
+<eng-data cg="97.5" f="78.06" m="92.5332" t="0.3"/>\r
+<eng-data cg="97.5" f="87.27" m="81.718" t="0.5"/>\r
+<eng-data cg="97.5" f="87.27" m="24.6297" t="1.5"/>\r
+<eng-data cg="97.5" f="82.64" m="13.5149" t="1.7"/>\r
+<eng-data cg="97.5" f="64.27" m="3.90467" t="1.9"/>\r
+<eng-data cg="97.5" f="18.37" m="1.20169" t="2."/>\r
+<eng-data cg="97.5" f="0." m="0." t="2.2"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; Aerotech G75J (Black Jack)\r
-;\r
-; AeroTech RMS-29/180 Easy Access Reloadable Motor Hardware.\r
-;\r
-; RASP.ENG file made from made from NAR or TMT published data.\r
-;\r
-; File produced May, 17 2004.\r
-;\r
-; The total impulse, peak thrust, average thrust and burn time are\r
-; the same as the averaged static test data from NAR or TMT files.\r
-;\r
-; The curve drawn with these data points is as accurate as could\r
-; could be made scaling the data from the curve on the TMT html\r
-; page. The file is 63 data points. NOT wRASP v1.6 compatible.\r
-;\r
-; The file was created by Stan Hemphill.\r
-; Contact at stanley_hemphill@hotmail.com.\r
-;\r
-; Motor Dia Len Delay Prop Gross Mfg\r
-G75J 29 194 1-3--4-6-7-9-10 0.114 0.236 AT\r
-0.0281 068.8604\r
-0.0380 078.6517\r
-0.0561 075.9230\r
-0.0660 073.0337\r
-0.0776 070.4655\r
-0.1139 069.3419\r
-0.1403 068.6998\r
-0.1667 067.5762\r
-0.1881 070.3050\r
-0.2013 069.0209\r
-0.2294 072.5522\r
-0.2541 076.4045\r
-0.2723 071.4286\r
-0.3102 076.2440\r
-0.3350 071.9101\r
-0.4208 075.6019\r
-0.4604 072.3917\r
-0.5215 079.2937\r
-0.5941 073.3547\r
-0.6436 080.0963\r
-0.7013 073.8363\r
-0.7393 076.4045\r
-0.7541 074.6388\r
-0.7657 077.3676\r
-0.7937 078.6517\r
-0.8036 077.0465\r
-0.8168 080.2568\r
-0.8267 075.2809\r
-0.8383 081.5409\r
-0.8581 075.7624\r
-0.8795 077.8491\r
-0.9340 074.1573\r
-0.9868 079.9358\r
-1.0380 076.7255\r
-1.0561 072.2311\r
-1.0941 078.8122\r
-1.1221 075.6019\r
-1.1502 080.8989\r
-1.1617 076.8860\r
-1.1848 080.0963\r
-1.1997 076.7255\r
-1.2327 078.8122\r
-1.2508 076.4045\r
-1.2871 082.5040\r
-1.3102 077.5281\r
-1.3267 081.8620\r
-1.3564 075.2809\r
-1.3729 080.0963\r
-1.4076 075.7624\r
-1.4884 079.9358\r
-1.5116 073.6758\r
-1.5297 081.0594\r
-1.5512 074.6388\r
-1.5611 080.8989\r
-1.6040 072.8732\r
-1.7211 075.6019\r
-1.7607 068.6998\r
-1.7789 070.1445\r
-1.8119 066.9342\r
-1.8267 070.7865\r
-1.8482 070.7865\r
-2.3878 000.0000\r
+++ /dev/null
-; Curve fit of AT Instruction sheet by C. Kobel 7/29/08\r
-G76G 29 124 4-7-10 0.06 0.147 AT\r
- 0.025 89.368\r
- 0.042 133.581\r
- 0.052 144.87\r
- 0.067 154.277\r
- 0.098 144.399\r
- 0.117 136.873\r
- 0.150 132.64\r
- 0.196 129.348\r
- 0.255 123.233\r
- 0.299 118.059\r
- 0.349 112.885\r
- 0.399 108.652\r
- 0.449 101.126\r
- 0.486 101.597\r
- 0.511 105.36\r
- 0.516 118.53\r
- 0.543 100.186\r
- 0.601 95.482\r
- 0.656 88.897\r
- 0.720 81.842\r
- 0.737 93.601\r
- 0.754 80.431\r
- 0.797 70.553\r
- 0.856 63.498\r
- 0.898 58.794\r
- 0.948 51.739\r
- 1.000 47.976\r
- 1.063 43.273\r
- 1.102 41.391\r
- 1.152 39.04\r
- 1.200 36.688\r
- 1.301 30.103\r
- 1.347 25.399\r
- 1.401 19.755\r
- 1.499 12.229\r
- 1.547 7.996\r
- 1.599 5.644\r
- 1.699 2.352\r
- 1.750 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Aerotech" code="G76G" Type="reloadable" dia="29." len="124." initWt="144."\r
+propWt="60." delays="4,7,10" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="57.226" peakThrust="149.304" throatDia="0." exitDia="0."\r
+Itot="114.503" burn-time="2." massFrac="41.67" Isp="194.6" tDiv="10" tStep="-1."\r
+tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+ <comments>From Official NAR Certification\r
+@File: G76G_Composite.txt, @Pts-I: 1001, @Pts-O: 33, @Sm: 4, @CO: 5%\r
+@TI: 114.4814, @TIa: 113.4881, @TIe: +0.01%, @ThMax: 149.6117, @ThAvg: 72.3776, @Tb: 1.568\r
+Mojave Green Formulation</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="60." cg="62."/>\r
+ <eng-data t="0." f="0.686899" m="60." cg="62."/>\r
+ <eng-data t="0.004" f="4.23776" m="59.9948" cg="62."/>\r
+ <eng-data t="0.006" f="9.67736" m="59.9875" cg="62."/>\r
+ <eng-data t="0.016" f="54.3647" m="59.8198" cg="62."/>\r
+ <eng-data t="0.03" f="98.111" m="59.2605" cg="62."/>\r
+ <eng-data t="0.034" f="108.445" m="59.044" cg="62."/>\r
+ <eng-data t="0.04" f="121.087" m="58.6832" cg="62."/>\r
+ <eng-data t="0.048" f="132.968" m="58.1507" cg="62."/>\r
+ <eng-data t="0.058" f="142.263" m="57.4296" cg="62."/>\r
+ <eng-data t="0.068" f="147.121" m="56.6714" cg="62."/>\r
+ <eng-data t="0.082" f="149.304" m="55.5841" cg="62."/>\r
+ <eng-data t="0.112" f="146.802" m="53.2567" cg="62."/>\r
+ <eng-data t="0.15" f="138.7" m="50.4142" cg="62."/>\r
+ <eng-data t="0.17" f="135.958" m="48.975" cg="62."/>\r
+ <eng-data t="0.376" f="112.155" m="35.5837" cg="62."/>\r
+ <eng-data t="0.466" f="103.018" m="30.5099" cg="62."/>\r
+ <eng-data t="0.482" f="104.376" m="29.6405" cg="62."/>\r
+ <eng-data t="0.56" f="92.5972" m="25.6152" cg="62."/>\r
+ <eng-data t="0.606" f="92.8117" m="23.3806" cg="62."/>\r
+ <eng-data t="0.644" f="84.1557" m="21.6187" cg="62."/>\r
+ <eng-data t="0.748" f="73.895" m="17.3121" cg="62."/>\r
+ <eng-data t="0.76" f="74.2399" m="16.8464" cg="62."/>\r
+ <eng-data t="0.79" f="69.6626" m="15.7153" cg="62."/>\r
+ <eng-data t="0.804" f="70.558" m="15.201" cg="62."/>\r
+ <eng-data t="0.822" f="66.7194" m="14.5536" cg="62."/>\r
+ <eng-data t="0.856" f="62.648" m="13.4012" cg="62."/>\r
+ <eng-data t="1.154" f="39.9734" m="5.38887" cg="62."/>\r
+ <eng-data t="1.3739" f="19.8986" m="1.9394" cg="62."/>\r
+ <eng-data t="1.4739" f="12.5124" m="1.09022" cg="62."/>\r
+ <eng-data t="1.5739" f="7.4133" m="0.568167" cg="62."/>\r
+ <eng-data t="1.7799" f="1.18956" m="0.103851" cg="62."/>\r
+ <eng-data t="1.9999" f="0.60939" m="0.000159661" cg="62."/>\r
+ <eng-data t="2.0009" f="0." m="0." cg="62."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; Aerotech G77R (Redline)\r
-;\r
-; AeroTech RMS-29/120 EZ Access Reloadable Motors (New! Hardware).\r
-; New AeroTech Redline Motor. Just announced on AeroTech's Website!\r
-; File produced 28 Feb 2005.\r
-;\r
-; The file was produced by scaling data points off the\r
-; thrust curve in the manufacturers catalog sheet.\r
-;\r
-; The motor is not yet on www.thrustcurve.org.\r
-; Hence the amateur file production.\r
-; The file was created by Stan Hemphill.\r
-; Contact at stanley_hemphill@hotmail.com.\r
-;\r
-; Motor Dia Len Delay Prop Gross Mfg\r
-G77R 29 150 4-6-8-9-10-12-13-15-17 0.0554 0.155 AT\r
-0.0132 014.8333\r
-0.0243 032.4479\r
-0.0331 046.3542\r
-0.0375 052.8438\r
-0.0463 056.5521\r
-0.0617 059.3333\r
-0.2580 073.2396\r
-0.6548 087.1458\r
-0.8709 089.0000\r
-0.8885 085.2917\r
-1.0252 086.2188\r
-1.0472 084.3646\r
-1.0715 086.2188\r
-1.1002 084.3646\r
-1.1332 085.2917\r
-1.1950 076.9479\r
-1.2104 076.0208\r
-1.2369 065.8229\r
-1.2611 043.5729\r
-1.2898 027.8125\r
-1.3317 012.0521\r
-1.3625 004.6354\r
-1.4000 000.0000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="191.68" Itot="104.139" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="77.716" burn-time="1.34" cgDiv="10" cgFix="1" cgStep="-1." code="G77R" delays="10" dia="29." exitDia="0." initWt="155." len="149.86" mDiv="10" mFix="1" mStep="-1." massFrac="35.74" mfg="Aerotech" peakThrust="96.892" propWt="55.4" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>G77R Data Entered by Tim Van Milligan\r
+For RockSim: www.RockSim.com\r
+Based on Aerotech's Reload Kit Instruction Sheet.\r
+Not Officially Approved by TRA or Aerotech\r
+</comments>\r
+<data>\r
+<eng-data cg="74.93" f="0." m="55.4" t="0."/>\r
+<eng-data cg="74.93" f="45.143" m="54.9197" t="0.04"/>\r
+<eng-data cg="74.93" f="53.951" m="54.1026" t="0.071"/>\r
+<eng-data cg="74.93" f="60.558" m="53.3411" t="0.096"/>\r
+<eng-data cg="74.93" f="68.265" m="51.8677" t="0.139"/>\r
+<eng-data cg="74.93" f="75.972" m="49.6041" t="0.198"/>\r
+<eng-data cg="74.93" f="83.679" m="45.5274" t="0.294"/>\r
+<eng-data cg="74.93" f="89.185" m="40.8375" t="0.396"/>\r
+<eng-data cg="74.93" f="91.387" m="35.362" t="0.51"/>\r
+<eng-data cg="74.93" f="93.589" m="30.9338" t="0.6"/>\r
+<eng-data cg="74.93" f="96.892" m="20.75" t="0.801"/>\r
+<eng-data cg="74.93" f="93.589" m="10.5661" t="1.002"/>\r
+<eng-data cg="74.93" f="89.185" m="5.80169" t="1.1"/>\r
+<eng-data cg="74.93" f="83.679" m="4.23837" t="1.134"/>\r
+<eng-data cg="74.93" f="77.073" m="2.78458" t="1.168"/>\r
+<eng-data cg="74.93" f="59.456" m="1.6588" t="1.199"/>\r
+<eng-data cg="74.93" f="34.132" m="0.737741" t="1.236"/>\r
+<eng-data cg="74.93" f="13.213" m="0.221415" t="1.277"/>\r
+<eng-data cg="74.93" f="0." m="0." t="1.34"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; @File: G78G_Typ.txt, @Pts-I: 1001, @Pts-O: 31, @Sm: 0, @CO: 5%\r
-; @TI: 109.776, @TIa: 109.5639, @TIe: 0.0%, @ThMax: 102.242, @ThAvg: 79.5671, @Tb: 1.377\r
-; Exported using ThrustCurveTool, www.ThrustGear.com\r
-G78G 29 146 4-7-10, 0.0597 0.125 AT/RCS\r
-0.0040 2.76203\r
-0.0060 34.7707\r
-0.0080 44.326\r
-0.01 41.2789\r
-0.012 28.5933\r
-0.014 27.3926\r
-0.016 38.0574\r
-0.02 47.7036\r
-0.022 48.2012\r
-0.03 56.4344\r
-0.042 61.4034\r
-0.06 65.883\r
-0.212 84.526\r
-0.266 88.9218\r
-0.404 95.5932\r
-0.43 98.9746\r
-0.466 100.5362\r
-0.58 102.242\r
-0.694 101.3187\r
-0.86 95.4526\r
-1.1 90.4186\r
-1.132 82.5618\r
-1.156 72.6383\r
-1.168 64.903\r
-1.194 42.3389\r
-1.216 28.3424\r
-1.226 24.9802\r
-1.2559 17.40051\r
-1.2859 13.04651\r
-1.3819 5.05295\r
-1.4719 0.0\r
--- /dev/null
+; @File: G78G_Typ.txt, @Pts-I: 1001, @Pts-O: 31, @Sm: 0, @CO: 5%\r
+; @TI: 109.776, @TIa: 109.5639, @TIe: 0.0%, @ThMax: 102.242, @ThAvg: 79.5671, @Tb: 1.377\r
+; Exported using ThrustCurveTool, www.ThrustGear.com\r
+G78G 29 146 4-7-10, 0.0597 0.125 AT/RCS\r
+0.0040 2.76203\r
+0.0060 34.7707\r
+0.0080 44.326\r
+0.01 41.2789\r
+0.012 28.5933\r
+0.014 27.3926\r
+0.016 38.0574\r
+0.02 47.7036\r
+0.022 48.2012\r
+0.03 56.4344\r
+0.042 61.4034\r
+0.06 65.883\r
+0.212 84.526\r
+0.266 88.9218\r
+0.404 95.5932\r
+0.43 98.9746\r
+0.466 100.5362\r
+0.58 102.242\r
+0.694 101.3187\r
+0.86 95.4526\r
+1.1 90.4186\r
+1.132 82.5618\r
+1.156 72.6383\r
+1.168 64.903\r
+1.194 42.3389\r
+1.216 28.3424\r
+1.226 24.9802\r
+1.2559 17.40051\r
+1.2859 13.04651\r
+1.3819 5.05295\r
+1.4719 0.0\r
-;\r
-;G79W Data Entered by Tim Van Milligan\r
-;For RockSim: www.RockSim.com\r
-;Based on TRA Certification Test date: June 13, 2004\r
-;Not Approved by TRA or Aerotech\r
-G79W 29 149.86 6-10-14 0.0609 0.154 AT\r
-0.015 7.157\r
-0.074 91.937\r
-0.09 91.387\r
-0.114 84.781\r
-0.145 84.23\r
-0.201 89.185\r
-0.291 94.69\r
-0.4 98.544\r
-0.6 99.645\r
-0.708 96.892\r
-0.8 93.038\r
-0.915 85.331\r
-1 77.624\r
-1.085 71.017\r
-1.175 68.265\r
-1.199 44.59\r
-1.28 22.021\r
-1.36 4.955\r
-1.42 0\r
+; Exported using ThrustCurveTool, www.ThrustGear.com \r
+; @File: G79_Ave.txt, @Pts-I: 1162, @Pts-O: 33, @Sm: 5, @CO: 5% \r
+; @TI: 106.4155, @TIa: 106.0632, @TIe: 0.0%, @ThMax: 82.1771, @ThAvg: 64.1443, @Tb: 1.659 \r
+G79 29 146 4,7,10 0.0601 0.124 Aerotech \r
+ 0.000 0.4562 \r
+ 0.014 1.1376 \r
+ 0.018 3.2129 \r
+ 0.022 6.2017 \r
+ 0.034 27.3705 \r
+ 0.040 33.5757 \r
+ 0.044 34.8528 \r
+ 0.062 33.5201 \r
+ 0.096 39.9175 \r
+ 0.128 56.9842 \r
+ 0.138 60.0917 \r
+ 0.182 59.6191 \r
+ 0.230 68.8942 \r
+ 0.266 71.3440 \r
+ 0.300 71.6246 \r
+ 0.360 75.8167 \r
+ 0.484 79.6244 \r
+ 0.516 78.6333 \r
+ 0.678 82.1075 \r
+ 0.700 78.8360 \r
+ 0.720 78.1790 \r
+ 0.772 79.5565 \r
+ 1.054 73.7176 \r
+ 1.086 71.1520 \r
+ 1.182 68.8555 \r
+ 1.420 57.2479 \r
+ 1.520 40.7567 \r
+ 1.562 30.5794 \r
+ 1.628 11.8028 \r
+ 1.652 7.1707 \r
+ 1.680 3.9601 \r
+ 1.738 1.6764 \r
+ 1.928 0.0000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="179.25" Itot="107.054" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="75.39" burn-time="1.42" cgDiv="10" cgFix="1" cgStep="-1." code="G79W" delays="6,10,14" dia="29." exitDia="0." initWt="154." len="149.86" mDiv="10" mFix="1" mStep="-1." massFrac="39.55" mfg="Aerotech" peakThrust="99.645" propWt="60.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>G79W Data Entered by Tim Van Milligan\r
+For RockSim: www.RockSim.com\r
+Based on TRA Certification Test date: June 13, 2004\r
+Not Approved by TRA or Aerotech\r
+</comments>\r
+<data>\r
+<eng-data cg="74.93" f="0." m="60.9" t="0."/>\r
+<eng-data cg="74.93" f="7.157" m="60.8695" t="0.015"/>\r
+<eng-data cg="74.93" f="91.937" m="59.2065" t="0.074"/>\r
+<eng-data cg="74.93" f="91.387" m="58.3722" t="0.09"/>\r
+<eng-data cg="74.93" f="84.781" m="57.1696" t="0.114"/>\r
+<eng-data cg="74.93" f="84.23" m="55.6793" t="0.145"/>\r
+<eng-data cg="74.93" f="89.185" m="52.9171" t="0.201"/>\r
+<eng-data cg="74.93" f="94.69" m="48.21" t="0.291"/>\r
+<eng-data cg="74.93" f="98.544" m="42.219" t="0.4"/>\r
+<eng-data cg="74.93" f="99.645" m="30.9446" t="0.6"/>\r
+<eng-data cg="74.93" f="96.892" m="24.9071" t="0.708"/>\r
+<eng-data cg="74.93" f="93.038" m="19.937" t="0.8"/>\r
+<eng-data cg="74.93" f="85.331" m="14.1025" t="0.915"/>\r
+<eng-data cg="74.93" f="77.624" m="10.1627" t="1."/>\r
+<eng-data cg="74.93" f="71.017" m="6.56901" t="1.085"/>\r
+<eng-data cg="74.93" f="68.265" m="3.00348" t="1.175"/>\r
+<eng-data cg="74.93" f="44.59" m="2.23308" t="1.199"/>\r
+<eng-data cg="74.93" f="22.021" m="0.698401" t="1.28"/>\r
+<eng-data cg="74.93" f="4.955" m="0.0845631" t="1.36"/>\r
+<eng-data cg="74.93" f="0." m="0." t="1.42"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="212.3" Itot="99.724" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="70.726" burn-time="1.41" cgDiv="10" cgFix="1" cgStep="-1." code="G80T" delays="4,7,10" dia="29." exitDia="0." initWt="116.1" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="41.26" mfg="Aerotech" peakThrust="110.761" propWt="47.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech G80T RASP.ENG file made by Tim Van Milligan\r
+For RockSim www.RockSim.com\r
+File Created March 2, 2005\r
+Thrust curve supplied by Aerotech for the molded case G80T motors.\r
+</comments>\r
+<data>\r
+<eng-data cg="62." f="0." m="47.9" t="0."/>\r
+<eng-data cg="62." f="110.761" m="47.4744" t="0.016"/>\r
+<eng-data cg="62." f="100.648" m="45.7989" t="0.049"/>\r
+<eng-data cg="62." f="98.537" m="38.8147" t="0.195"/>\r
+<eng-data cg="62." f="96.425" m="25.8447" t="0.472"/>\r
+<eng-data cg="62." f="90.091" m="18.5433" t="0.635"/>\r
+<eng-data cg="62." f="82.348" m="11.7928" t="0.798"/>\r
+<eng-data cg="62." f="63.345" m="5.07471" t="0.99"/>\r
+<eng-data cg="62." f="38.711" m="1.86387" t="1.121"/>\r
+<eng-data cg="62." f="18.3" m="0.576826" t="1.215"/>\r
+<eng-data cg="62." f="5.56" m="0.164243" t="1.287"/>\r
+<eng-data cg="62." f="0." m="0." t="1.41"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Aerotech G80 RASP.ENG file made from NAR published data\r
-; File produced July 4, 2000\r
-; Note: This is for the 116N-sec G80T produced before Sept. 2006\r
-G80 29 124 4-7-10 0.0574 0.1049 A\r
- 0.0060 101.291\r
- 0.013 105.18\r
- 0.031 103.473\r
- 0.038 104.069\r
- 0.067 99.803\r
- 0.103 96.906\r
- 0.181 94.733\r
- 0.271 94.039\r
- 0.303 96.985\r
- 0.367 95.547\r
- 0.428 94.842\r
- 0.456 97.055\r
- 0.463 92.65\r
- 0.51 94.872\r
- 0.596 93.444\r
- 0.606 95.646\r
- 0.624 91.985\r
- 0.635 95.656\r
- 0.646 91.995\r
- 0.696 90.547\r
- 0.846 85.477\r
- 0.96 80.388\r
- 1.071 74.564\r
- 1.207 62.878\r
- 1.296 52.639\r
- 1.35 37.252\r
- 1.382 20.397\r
- 1.418 10.139\r
- 1.457 4.281\r
- 1.5 0.0\r
+++ /dev/null
-; AeroTech H112J\r
-; Copyright Tripoli Motor Testing 1999 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-H112J 38 202 0 0.187712 0.379456 AT\r
- 0.064 85.431\r
- 0.194 101.938\r
- 0.324 101.897\r
- 0.454 102.839\r
- 0.584 104.479\r
- 0.715 103.845\r
- 0.845 103.439\r
- 0.975 104.286\r
- 1.106 104.922\r
- 1.236 104.390\r
- 1.367 102.768\r
- 1.497 102.237\r
- 1.627 100.032\r
- 1.757 98.345\r
- 1.888 94.560\r
- 2.018 89.018\r
- 2.148 82.857\r
- 2.279 77.685\r
- 2.409 72.373\r
- 2.540 67.041\r
- 2.670 59.764\r
- 2.800 37.616\r
- 2.930 14.457\r
- 3.060 4.642\r
- 3.192 1.818\r
- 3.323 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="152.65" Itot="280.685" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="82.554" burn-time="3.4" cgDiv="10" cgFix="1" cgStep="-1." code="H112J" delays="6,10,14" dia="38." exitDia="0." initWt="384.8" len="191." mDiv="10" mFix="1" mStep="-1." massFrac="48.73" mfg="Aerotech" peakThrust="126.62" propWt="187.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Data Entered by Tim Van Milligan\r
+For RockSim Users. http://www.rocksim.com\r
+Based on Aerotech's RMS 38/240-360 Black Jack Instr. Sheet\r
+</comments>\r
+<data>\r
+<eng-data cg="95.5" f="0." m="187.5" t="0."/>\r
+<eng-data cg="95.5" f="120.014" m="180.665" t="0.1705"/>\r
+<eng-data cg="95.5" f="126.62" m="178.235" t="0.2"/>\r
+<eng-data cg="95.5" f="109.003" m="176.347" t="0.224"/>\r
+<eng-data cg="95.5" f="106.801" m="172.454" t="0.278"/>\r
+<eng-data cg="95.5" f="107.902" m="165.283" t="0.378"/>\r
+<eng-data cg="95.5" f="113.408" m="156.117" t="0.502"/>\r
+<eng-data cg="95.5" f="103.498" m="120.328" t="0.996"/>\r
+<eng-data cg="95.5" f="103.498" m="85.552" t="1.499"/>\r
+<eng-data cg="95.5" f="96.892" m="70.0239" t="1.731"/>\r
+<eng-data cg="95.5" f="92.487" m="51.9335" t="2.017"/>\r
+<eng-data cg="95.5" f="73.77" m="25.3343" t="2.496"/>\r
+<eng-data cg="95.5" f="42.94" m="5.76554" t="2.998"/>\r
+<eng-data cg="95.5" f="0." m="0." t="3.4"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech H123W\r
-; Copyright Tripoli Motor Testing 1999 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-H123W 38 154 0 0.126336 0.278656 AT\r
- 0.047 96.764\r
- 0.143 146.256\r
- 0.239 150.699\r
- 0.334 152.496\r
- 0.430 151.248\r
- 0.526 149.875\r
- 0.622 150.200\r
- 0.718 149.176\r
- 0.814 144.858\r
- 0.909 143.536\r
- 1.005 141.414\r
- 1.101 135.125\r
- 1.198 125.288\r
- 1.295 114.035\r
- 1.391 101.556\r
- 1.486 90.175\r
- 1.582 78.694\r
- 1.678 66.364\r
- 1.774 54.260\r
- 1.870 46.872\r
- 1.966 38.186\r
- 2.061 22.737\r
- 2.157 13.478\r
- 2.253 7.587\r
- 2.350 5.252\r
- 2.447 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="172.45" Itot="211.4" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="81.308" burn-time="2.6" cgDiv="10" cgFix="1" cgStep="-1." code="H123W" delays="6,10,14" dia="38." exitDia="0." initWt="293.3" len="154." mDiv="10" mFix="1" mStep="-1." massFrac="42.62" mfg="Aerotech" peakThrust="138.42" propWt="125." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="77." f="0." m="125." t="0."/>\r
+<eng-data cg="77." f="138.42" m="125." t="0."/>\r
+<eng-data cg="77." f="116.45" m="109.93" t="0.2"/>\r
+<eng-data cg="77." f="116.45" m="82.3872" t="0.6"/>\r
+<eng-data cg="77." f="112.18" m="75.6278" t="0.7"/>\r
+<eng-data cg="77." f="107.82" m="69.1235" t="0.8"/>\r
+<eng-data cg="77." f="86.29" m="40.4295" t="1.3"/>\r
+<eng-data cg="77." f="81.93" m="30.4827" t="1.5"/>\r
+<eng-data cg="77." f="64.72" m="17.4757" t="1.8"/>\r
+<eng-data cg="77." f="47.46" m="7.526" t="2.1"/>\r
+<eng-data cg="77." f="43.15" m="4.84714" t="2.2"/>\r
+<eng-data cg="77." f="30.2" m="2.67857" t="2.3"/>\r
+<eng-data cg="77." f="0." m="0." t="2.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
; AeroTech H125W\r
-; Copyright Tripoli Motor Testing 1997 (www.tripoli.org)\r
+; converted from TMT test stand data 1997 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
H125W 29 330 14 0.18816 0.32256 AT\r
0.053 275.994\r
; AeroTech H128W\r
-; Copyright Tripoli Motor Testing 1997 (www.tripoli.org)\r
+; converted from TMT test stand data 1997 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
H128W 29 194 14 0.09408 0.2016 AT\r
0.024 102.423\r
+++ /dev/null
-; AeroTech H148R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-H148R 38 152 0 0.14784 0.30912 AT\r
- 0.027 77.232\r
- 0.088 174.296\r
- 0.148 185.046\r
- 0.208 190.458\r
- 0.268 192.497\r
- 0.327 191.996\r
- 0.388 188.790\r
- 0.448 187.548\r
- 0.509 182.697\r
- 0.570 178.151\r
- 0.630 172.906\r
- 0.690 169.607\r
- 0.750 164.510\r
- 0.810 158.375\r
- 0.870 153.019\r
- 0.930 146.810\r
- 0.991 139.443\r
- 1.053 132.001\r
- 1.112 123.271\r
- 1.173 112.559\r
- 1.233 104.737\r
- 1.292 97.657\r
- 1.353 94.932\r
- 1.413 60.644\r
- 1.474 13.007\r
- 1.535 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="145.6" Itot="214.18" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="142.786" burn-time="1.5" cgDiv="10" cgFix="1" cgStep="-1." code="H148R" delays="6,11,14" dia="38." exitDia="0." initWt="313." len="152." mDiv="10" mFix="1" mStep="-1." massFrac="47.92" mfg="Aerotech" peakThrust="192.5" propWt="150." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="76." f="0." m="150." t="0."/>\r
+<eng-data cg="76." f="77.23" m="149.189" t="0.03"/>\r
+<eng-data cg="76." f="174.3" m="143.904" t="0.09"/>\r
+<eng-data cg="76." f="185.05" m="136.354" t="0.15"/>\r
+<eng-data cg="76." f="190.46" m="128.464" t="0.21"/>\r
+<eng-data cg="76." f="192.5" m="120.418" t="0.27"/>\r
+<eng-data cg="76." f="192." m="112.34" t="0.33"/>\r
+<eng-data cg="76." f="188.79" m="104.339" t="0.39"/>\r
+<eng-data cg="76." f="187.55" m="96.432" t="0.45"/>\r
+<eng-data cg="76." f="182.7" m="88.6529" t="0.51"/>\r
+<eng-data cg="76." f="178.15" m="81.0713" t="0.57"/>\r
+<eng-data cg="76." f="172.91" m="73.6954" t="0.63"/>\r
+<eng-data cg="76." f="169.61" m="66.4989" t="0.69"/>\r
+<eng-data cg="76." f="164.51" m="59.4789" t="0.75"/>\r
+<eng-data cg="76." f="158.38" m="52.6948" t="0.81"/>\r
+<eng-data cg="76." f="153.02" m="46.1522" t="0.87"/>\r
+<eng-data cg="76." f="146.81" m="39.8526" t="0.93"/>\r
+<eng-data cg="76." f="139.44" m="33.8384" t="0.99"/>\r
+<eng-data cg="76." f="132." m="28.1353" t="1.05"/>\r
+<eng-data cg="76." f="123.27" m="22.772" t="1.11"/>\r
+<eng-data cg="76." f="112.56" m="17.8171" t="1.17"/>\r
+<eng-data cg="76." f="104.74" m="13.2516" t="1.23"/>\r
+<eng-data cg="76." f="97.66" m="8.99907" t="1.29"/>\r
+<eng-data cg="76." f="94.93" m="4.95268" t="1.35"/>\r
+<eng-data cg="76." f="60.64" m="1.68409" t="1.41"/>\r
+<eng-data cg="76." f="13.01" m="0.136673" t="1.47"/>\r
+<eng-data cg="76." f="0." m="0." t="1.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech H165R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-H165R 29 194 0 0.0896 0.2016 AT\r
- 0.018 55.047\r
- 0.059 157.258\r
- 0.101 168.509\r
- 0.144 173.219\r
- 0.186 179.237\r
- 0.229 183.947\r
- 0.271 187.872\r
- 0.314 188.134\r
- 0.356 188.919\r
- 0.399 190.488\r
- 0.441 187.349\r
- 0.484 189.180\r
- 0.525 186.547\r
- 0.566 185.517\r
- 0.609 180.807\r
- 0.651 177.667\r
- 0.694 170.602\r
- 0.736 167.201\r
- 0.779 158.828\r
- 0.821 155.688\r
- 0.864 153.333\r
- 0.906 136.325\r
- 0.949 73.526\r
- 0.991 20.671\r
- 1.034 4.448\r
- 1.076 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="180.28" Itot="160.882" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="153.221" burn-time="1.05" cgDiv="10" cgFix="1" cgStep="-1." code="H165R" delays="10,14" dia="29." exitDia="0." initWt="204." len="194." mDiv="10" mFix="1" mStep="-1." massFrac="44.61" mfg="Aerotech" peakThrust="190.49" propWt="91." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="97." f="0." m="91." t="0."/>\r
+<eng-data cg="97." f="55.05" m="90.6886" t="0.02"/>\r
+<eng-data cg="97." f="157.26" m="88.2868" t="0.06"/>\r
+<eng-data cg="97." f="168.51" m="84.6015" t="0.1"/>\r
+<eng-data cg="97." f="173.22" m="80.7356" t="0.14"/>\r
+<eng-data cg="97." f="179.24" m="75.7516" t="0.19"/>\r
+<eng-data cg="97." f="183.95" m="71.6429" t="0.23"/>\r
+<eng-data cg="97." f="187.87" m="67.4367" t="0.27"/>\r
+<eng-data cg="97." f="188.13" m="63.1831" t="0.31"/>\r
+<eng-data cg="97." f="188.92" m="57.8513" t="0.36"/>\r
+<eng-data cg="97." f="190.49" m="53.5592" t="0.4"/>\r
+<eng-data cg="97." f="187.35" m="49.2849" t="0.44"/>\r
+<eng-data cg="97." f="189.18" m="45.0253" t="0.48"/>\r
+<eng-data cg="97." f="186.55" m="39.7122" t="0.53"/>\r
+<eng-data cg="97." f="185.52" m="35.5031" t="0.57"/>\r
+<eng-data cg="97." f="180.81" m="31.3589" t="0.61"/>\r
+<eng-data cg="97." f="177.67" m="27.3036" t="0.65"/>\r
+<eng-data cg="97." f="170.6" m="23.3637" t="0.69"/>\r
+<eng-data cg="97." f="167.2" m="18.587" t="0.74"/>\r
+<eng-data cg="97." f="158.83" m="14.8987" t="0.78"/>\r
+<eng-data cg="97." f="155.69" m="11.3407" t="0.82"/>\r
+<eng-data cg="97." f="153.33" m="7.84483" t="0.86"/>\r
+<eng-data cg="97." f="136.32" m="3.74895" t="0.91"/>\r
+<eng-data cg="97." f="73.53" m="1.37499" t="0.95"/>\r
+<eng-data cg="97." f="20.67" m="0.309344" t="0.99"/>\r
+<eng-data cg="97." f="4.45" m="0.0251706" t="1.03"/>\r
+<eng-data cg="97." f="0." m="0." t="1.05"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
; AeroTech H180W\r
-; Copyright Tripoli Motor Testing 1997 (www.tripoli.org)\r
+; converted from TMT test stand data 1997 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
H180W 29 238 6 0.12096 0.2464 AT\r
0.024 149.374\r
+++ /dev/null
-; AeroTech H210R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-H210R 29 238 0 0.12096 0.2464 AT\r
- 0.019 105.923\r
- 0.059 211.290\r
- 0.099 219.770\r
- 0.139 229.639\r
- 0.179 235.082\r
- 0.220 241.594\r
- 0.260 242.706\r
- 0.300 245.347\r
- 0.341 249.100\r
- 0.381 253.410\r
- 0.421 258.553\r
- 0.461 260.221\r
- 0.502 257.997\r
- 0.543 259.248\r
- 0.583 256.607\r
- 0.623 252.436\r
- 0.663 245.056\r
- 0.704 219.909\r
- 0.744 209.344\r
- 0.784 200.587\r
- 0.824 193.565\r
- 0.865 184.323\r
- 0.905 153.881\r
- 0.945 58.244\r
- 0.986 13.210\r
- 1.027 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="175.59" Itot="210.078" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="207.998" burn-time="1.01" cgDiv="10" cgFix="1" cgStep="-1." code="H210R" delays="10,1000" dia="29." exitDia="0." initWt="249." len="238." mDiv="10" mFix="1" mStep="-1." massFrac="49." mfg="Aerotech" peakThrust="260.22" propWt="122." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="119." f="0." m="122." t="0."/>\r
+<eng-data cg="119." f="105.92" m="121.385" t="0.02"/>\r
+<eng-data cg="119." f="211.29" m="117.701" t="0.06"/>\r
+<eng-data cg="119." f="219.77" m="112.694" t="0.1"/>\r
+<eng-data cg="119." f="229.64" m="107.474" t="0.14"/>\r
+<eng-data cg="119." f="235.08" m="102.077" t="0.18"/>\r
+<eng-data cg="119." f="241.59" m="96.5402" t="0.22"/>\r
+<eng-data cg="119." f="242.71" m="90.9152" t="0.26"/>\r
+<eng-data cg="119." f="245.35" m="85.2465" t="0.3"/>\r
+<eng-data cg="119." f="249.1" m="79.5036" t="0.34"/>\r
+<eng-data cg="119." f="253.41" m="73.6671" t="0.38"/>\r
+<eng-data cg="119." f="258.55" m="67.7208" t="0.42"/>\r
+<eng-data cg="119." f="260.22" m="61.6955" t="0.46"/>\r
+<eng-data cg="119." f="258." m="55.6765" t="0.5"/>\r
+<eng-data cg="119." f="259.25" m="49.6688" t="0.54"/>\r
+<eng-data cg="119." f="256.61" m="43.6772" t="0.58"/>\r
+<eng-data cg="119." f="252.44" m="37.7647" t="0.62"/>\r
+<eng-data cg="119." f="245.06" m="31.9864" t="0.66"/>\r
+<eng-data cg="119." f="219.91" m="26.5859" t="0.7"/>\r
+<eng-data cg="119." f="209.34" m="21.6003" t="0.74"/>\r
+<eng-data cg="119." f="200.59" m="16.8391" t="0.78"/>\r
+<eng-data cg="119." f="193.57" m="12.261" t="0.82"/>\r
+<eng-data cg="119." f="184.32" m="7.87196" t="0.86"/>\r
+<eng-data cg="119." f="153.88" m="2.96184" t="0.91"/>\r
+<eng-data cg="119." f="58.24" m="1.11405" t="0.94"/>\r
+<eng-data cg="119." f="13.21" m="0.0767152" t="0.99"/>\r
+<eng-data cg="119." f="0." m="0." t="1.01"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-H220T 29 239 6-10-14 0.1064 0.2386 AT\r
-0 314.1\r
-0.1 236.61\r
-0.2 269.23\r
-0.3 261.06\r
-0.4 252.9\r
-0.72 252.9\r
-0.8 112.58\r
-0.9 9.78\r
-0.96 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="198.38" Itot="206.999" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="215.624" burn-time="0.96" cgDiv="10" cgFix="1" cgStep="-1." code="H220T" delays="6,10,14" dia="29." exitDia="0." initWt="238.6" len="239." mDiv="10" mFix="1" mStep="-1." massFrac="44.59" mfg="Aerotech" peakThrust="314.1" propWt="106.4" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="119.5" f="0." m="106.4" t="0."/>\r
+<eng-data cg="119.5" f="314.1" m="106.4" t="0."/>\r
+<eng-data cg="119.5" f="236.61" m="92.2464" t="0.1"/>\r
+<eng-data cg="119.5" f="269.23" m="79.246" t="0.2"/>\r
+<eng-data cg="119.5" f="261.06" m="65.6172" t="0.3"/>\r
+<eng-data cg="119.5" f="252.9" m="52.4081" t="0.4"/>\r
+<eng-data cg="119.5" f="252.9" m="10.81" t="0.72"/>\r
+<eng-data cg="119.5" f="112.58" m="3.29554" t="0.8"/>\r
+<eng-data cg="119.5" f="9.78" m="0.150811" t="0.9"/>\r
+<eng-data cg="119.5" f="0." m="0." t="0.96"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
; AeroTech H238T\r
-; Copyright Tripoli Motor Testing 1997 (www.tripoli.org)\r
+; converted from TMT test stand data 1997 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
H238T 29 194 6 0.08064 0.18816 AT\r
0.019 173.100\r
+++ /dev/null
-; AeroTech H242T\r
-; Copyright Tripoli Motor Testing 1997 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-H242T 38 152 10 0.11648 0.2688 AT\r
- 0.030 164.060\r
- 0.093 197.516\r
- 0.155 204.324\r
- 0.218 208.970\r
- 0.280 211.481\r
- 0.343 211.261\r
- 0.405 209.291\r
- 0.468 208.438\r
- 0.531 206.707\r
- 0.595 203.967\r
- 0.657 198.175\r
- 0.720 192.137\r
- 0.782 186.840\r
- 0.845 180.802\r
- 0.907 174.635\r
- 0.970 165.581\r
- 1.033 159.726\r
- 1.097 151.690\r
- 1.159 144.167\r
- 1.222 138.550\r
- 1.284 119.114\r
- 1.347 69.055\r
- 1.409 21.396\r
- 1.472 3.473\r
- 1.535 0.594\r
- 1.599 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="215.56" Itot="234.218" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="195.182" burn-time="1.2" cgDiv="10" cgFix="1" cgStep="-1." code="H242T" delays="6,10,14" dia="38." exitDia="0." initWt="279.1" len="154." mDiv="10" mFix="1" mStep="-1." massFrac="39.7" mfg="Aerotech" peakThrust="286.05" propWt="110.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="77." f="0." m="110.8" t="0."/>\r
+<eng-data cg="77." f="286.05" m="110.8" t="0."/>\r
+<eng-data cg="77." f="255.09" m="98.0003" t="0.1"/>\r
+<eng-data cg="77." f="241.88" m="74.4906" t="0.3"/>\r
+<eng-data cg="77." f="241.88" m="63.0481" t="0.4"/>\r
+<eng-data cg="77." f="233.16" m="51.8119" t="0.5"/>\r
+<eng-data cg="77." f="211.15" m="30.7933" t="0.7"/>\r
+<eng-data cg="77." f="193.53" m="21.2213" t="0.8"/>\r
+<eng-data cg="77." f="171.51" m="12.587" t="0.9"/>\r
+<eng-data cg="77." f="118.76" m="5.72122" t="1."/>\r
+<eng-data cg="77." f="61.56" m="1.45609" t="1.1"/>\r
+<eng-data cg="77." f="0." m="0." t="1.2"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech H242T\r
-; Copyright Tripoli Motor Testing 1999 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-H242T 38 154 0 0.114688 0.264768 AT\r
- 0.025 207.058\r
- 0.077 237.941\r
- 0.129 240.171\r
- 0.181 241.906\r
- 0.234 246.425\r
- 0.287 245.971\r
- 0.340 247.210\r
- 0.392 246.516\r
- 0.445 245.710\r
- 0.498 244.881\r
- 0.550 242.997\r
- 0.602 240.518\r
- 0.655 235.271\r
- 0.708 229.464\r
- 0.760 222.871\r
- 0.813 216.278\r
- 0.866 206.959\r
- 0.919 195.458\r
- 0.971 184.255\r
- 1.023 174.490\r
- 1.076 170.067\r
- 1.129 99.588\r
- 1.181 25.281\r
- 1.233 12.839\r
- 1.286 7.769\r
- 1.340 0.000\r
+++ /dev/null
-;I don't know that \r
-;these ejection \r
-;delays are correct. \r
-;This was made \r
-;using the Aerotech \r
-;test thrust curves. \r
-;By Tobin Yehle, \r
-;11/11/07.\r
-H250G 29 228.93 0-6-10-14 0.1163 0.256 Aerotech \r
-0.00250627 88.6915\r
-0.0125313 177.383\r
-0.0300752 279.719\r
-0.0726817 311.103\r
-0.145363 320.654\r
-0.24812 311.103\r
-0.308271 297.458\r
-0.398496 282.448\r
-0.45614 270.168\r
-0.593985 238.785\r
-0.691729 221.047\r
-0.799499 218.318\r
-0.83208 210.131\r
-0.844612 189.663\r
-0.907268 13.6449\r
-0.92 0\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Aerotech" code="H250G" Type="reloadable" dia="29." len="228.93"\r
+initWt="256." propWt="116.3" delays="0,6,10,14" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="251.105" peakThrust="320.655" throatDia="0."\r
+exitDia="0." Itot="231.017" burn-time="0.92" massFrac="0." Isp="0." tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>I don't know that \r
+these ejection \r
+delays are correct. \r
+This was made \r
+using the Aerotech \r
+test thrust curves. \r
+By Tobin Yehle, \r
+11/11/07.</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="0." cg="0."/>\r
+ <eng-data t="0.00250627" f="88.6915" m="0." cg="0."/>\r
+ <eng-data t="0.0125313" f="177.383" m="0." cg="0."/>\r
+ <eng-data t="0.0300752" f="279.719" m="0." cg="0."/>\r
+ <eng-data t="0.0726817" f="311.103" m="0." cg="0."/>\r
+ <eng-data t="0.145363" f="320.654" m="0." cg="0."/>\r
+ <eng-data t="0.24812" f="311.103" m="0." cg="0."/>\r
+ <eng-data t="0.308271" f="297.458" m="0." cg="0."/>\r
+ <eng-data t="0.398496" f="282.448" m="0." cg="0."/>\r
+ <eng-data t="0.45614" f="270.168" m="0." cg="0."/>\r
+ <eng-data t="0.593985" f="238.785" m="0." cg="0."/>\r
+ <eng-data t="0.691729" f="221.047" m="0." cg="0."/>\r
+ <eng-data t="0.799499" f="218.318" m="0." cg="0."/>\r
+ <eng-data t="0.83208" f="210.131" m="0." cg="0."/>\r
+ <eng-data t="0.844612" f="189.663" m="0." cg="0."/>\r
+ <eng-data t="0.907268" f="13.6449" m="0." cg="0."/>\r
+ <eng-data t="0.92" f="0." m="0." cg="0."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech H268R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-H268R 29 333 0 0.18368 0.3584 AT\r
- 0.022 268.095\r
- 0.069 332.446\r
- 0.116 312.429\r
- 0.164 306.810\r
- 0.211 305.757\r
- 0.259 306.576\r
- 0.306 312.546\r
- 0.354 319.687\r
- 0.401 321.234\r
- 0.448 320.974\r
- 0.495 321.208\r
- 0.542 321.794\r
- 0.590 323.315\r
- 0.638 322.847\r
- 0.685 307.044\r
- 0.732 291.593\r
- 0.779 277.713\r
- 0.826 267.127\r
- 0.874 257.529\r
- 0.921 252.846\r
- 0.969 222.645\r
- 1.016 159.668\r
- 1.064 108.747\r
- 1.111 52.091\r
- 1.159 15.569\r
- 1.207 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="171.65" Itot="309.73" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="262.483" burn-time="1.18" cgDiv="10" cgFix="1" cgStep="-1." code="H268R" delays="10,14,1000" dia="29." exitDia="0." initWt="362." len="333." mDiv="10" mFix="1" mStep="-1." massFrac="50.83" mfg="Aerotech" peakThrust="332.45" propWt="184." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="166.5" f="0." m="184." t="0."/>\r
+<eng-data cg="166.5" f="268.1" m="182.407" t="0.02"/>\r
+<eng-data cg="166.5" f="332.45" m="173.488" t="0.07"/>\r
+<eng-data cg="166.5" f="312.43" m="163.911" t="0.12"/>\r
+<eng-data cg="166.5" f="306.81" m="156.553" t="0.16"/>\r
+<eng-data cg="166.5" f="305.76" m="147.456" t="0.21"/>\r
+<eng-data cg="166.5" f="306.58" m="138.361" t="0.26"/>\r
+<eng-data cg="166.5" f="312.55" m="129.166" t="0.31"/>\r
+<eng-data cg="166.5" f="319.69" m="121.654" t="0.35"/>\r
+<eng-data cg="166.5" f="321.23" m="112.136" t="0.4"/>\r
+<eng-data cg="166.5" f="320.97" m="102.598" t="0.45"/>\r
+<eng-data cg="166.5" f="321.21" m="93.0605" t="0.5"/>\r
+<eng-data cg="166.5" f="321.79" m="85.4208" t="0.54"/>\r
+<eng-data cg="166.5" f="323.32" m="75.8399" t="0.59"/>\r
+<eng-data cg="166.5" f="322.85" m="66.2432" t="0.64"/>\r
+<eng-data cg="166.5" f="307.04" m="56.8883" t="0.69"/>\r
+<eng-data cg="166.5" f="291.59" m="49.7758" t="0.73"/>\r
+<eng-data cg="166.5" f="277.71" m="41.3207" t="0.78"/>\r
+<eng-data cg="166.5" f="267.13" m="33.229" t="0.83"/>\r
+<eng-data cg="166.5" f="257.53" m="26.9953" t="0.87"/>\r
+<eng-data cg="166.5" f="252.85" m="19.4153" t="0.92"/>\r
+<eng-data cg="166.5" f="222.65" m="12.3534" t="0.97"/>\r
+<eng-data cg="166.5" f="159.67" m="6.67528" t="1.02"/>\r
+<eng-data cg="166.5" f="108.75" m="3.4861" t="1.06"/>\r
+<eng-data cg="166.5" f="52.09" m="1.09736" t="1.11"/>\r
+<eng-data cg="166.5" f="15.57" m="0.092496" t="1.16"/>\r
+<eng-data cg="166.5" f="0." m="0." t="1.18"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech H45W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-H45W 38 194 0 0.193984 0.294784 AT\r
- 0.141 62.554\r
- 0.424 63.504\r
- 0.707 65.913\r
- 0.992 68.370\r
- 1.276 69.315\r
- 1.559 68.523\r
- 1.843 67.231\r
- 2.127 65.705\r
- 2.411 63.154\r
- 2.695 59.210\r
- 2.979 55.600\r
- 3.264 50.790\r
- 3.547 45.237\r
- 3.830 39.835\r
- 4.115 34.562\r
- 4.399 29.213\r
- 4.682 24.720\r
- 4.967 20.616\r
- 5.251 17.475\r
- 5.534 14.498\r
- 5.818 12.697\r
- 6.102 10.792\r
- 6.386 9.229\r
- 6.670 7.754\r
- 6.954 6.075\r
- 7.239 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="196.19" Itot="319.77" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="44.975" burn-time="7.11" cgDiv="10" cgFix="1" cgStep="-1." code="H45W" delays="10,15" dia="38." exitDia="0." initWt="320." len="191." mDiv="10" mFix="1" mStep="-1." massFrac="51.94" mfg="Aerotech" peakThrust="128." propWt="166.2" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="95.5" f="0." m="166.2" t="0."/>\r
+<eng-data cg="95.5" f="89." m="165.044" t="0.05"/>\r
+<eng-data cg="95.5" f="128." m="139.667" t="0.5"/>\r
+<eng-data cg="95.5" f="63." m="128.251" t="0.73"/>\r
+<eng-data cg="95.5" f="50." m="46.9073" t="3.5"/>\r
+<eng-data cg="95.5" f="0." m="0." t="7.11"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech H55W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-H55W 29 191 0 0.09856 0.18816 AT\r
- 0.052 92.752\r
- 0.159 98.019\r
- 0.268 95.821\r
- 0.375 96.162\r
- 0.482 97.146\r
- 0.591 96.927\r
- 0.699 95.915\r
- 0.806 94.447\r
- 0.914 92.001\r
- 1.022 88.756\r
- 1.129 86.970\r
- 1.236 84.072\r
- 1.345 80.172\r
- 1.453 74.343\r
- 1.560 64.990\r
- 1.668 46.380\r
- 1.776 32.835\r
- 1.883 25.734\r
- 1.991 19.920\r
- 2.099 16.229\r
- 2.207 13.059\r
- 2.315 10.451\r
- 2.422 7.700\r
- 2.530 5.696\r
- 2.639 3.979\r
- 2.747 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="246.13" Itot="200.1" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="54.973" burn-time="3.64" cgDiv="10" cgFix="1" cgStep="-1." code="H55W" delays="6,10,14" dia="29." exitDia="0." initWt="140." len="172." mDiv="10" mFix="1" mStep="-1." massFrac="59.21" mfg="Aerotech" peakThrust="69." propWt="82.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="86." f="0." m="82.9" t="0."/>\r
+<eng-data cg="86." f="69." m="81.4707" t="0.1"/>\r
+<eng-data cg="86." f="69." m="19.7245" t="2.26"/>\r
+<eng-data cg="86." f="0." m="0." t="3.64"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; 38-240\r
-; Greg Gardner - 09/15/06\r
-H669N 38 152 0 0.096 0.252 AT\r
-0.003 141\r
-0.006 523\r
-0.009 934\r
-0.012 1178\r
-0.016 926\r
-0.019 684\r
-0.022 487\r
-0.025 415\r
-0.028 622\r
-0.031 801\r
-0.0325 906\r
-0.034 866\r
-0.037 755\r
-0.04 737\r
-0.043 666\r
-0.047 737\r
-0.0485 802\r
-0.05 755\r
-0.053 791\r
-0.056 765\r
-0.059 755\r
-0.062 747\r
-0.069 737\r
-0.075 761\r
-0.082 755\r
-0.088 729\r
-0.093 741\r
-0.1 751\r
-0.2 703\r
-0.25 640\r
-0.3 586\r
-0.306 584\r
-0.309 576\r
-0.312 506\r
-0.318 292\r
-0.325 93\r
-0.329 0\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="233.42" Itot="219.749" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="667.931" burn-time="0.33" cgDiv="10" cgFix="1" cgStep="-1." code="H669N" delays="1000" dia="38." exitDia="0." initWt="252." len="152." mDiv="10" mFix="1" mStep="-1." massFrac="38.1" mfg="Aerotech" peakThrust="1178." propWt="96." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Greg Gardner - 09/15/06</comments>\r
+<data>\r
+<eng-data cg="76." f="0." m="96." t="0."/>\r
+<eng-data cg="76." f="141." m="95.9076" t="0.003"/>\r
+<eng-data cg="76." f="523." m="95.4725" t="0.006"/>\r
+<eng-data cg="76." f="934." m="94.5177" t="0.009"/>\r
+<eng-data cg="76." f="1178." m="93.1338" t="0.012"/>\r
+<eng-data cg="76." f="926." m="91.2954" t="0.016"/>\r
+<eng-data cg="76." f="684." m="90.2404" t="0.019"/>\r
+<eng-data cg="76." f="487." m="89.4731" t="0.022"/>\r
+<eng-data cg="76." f="415." m="88.882" t="0.025"/>\r
+<eng-data cg="76." f="622." m="88.2025" t="0.028"/>\r
+<eng-data cg="76." f="801." m="87.27" t="0.031"/>\r
+<eng-data cg="76." f="906." m="86.7107" t="0.0325"/>\r
+<eng-data cg="76." f="866." m="86.1301" t="0.034"/>\r
+<eng-data cg="76." f="755." m="85.0679" t="0.037"/>\r
+<eng-data cg="76." f="737." m="84.0902" t="0.04"/>\r
+<eng-data cg="76." f="666." m="83.1708" t="0.043"/>\r
+<eng-data cg="76." f="737." m="81.945" t="0.047"/>\r
+<eng-data cg="76." f="802." m="81.4407" t="0.0485"/>\r
+<eng-data cg="76." f="755." m="80.9306" t="0.05"/>\r
+<eng-data cg="76." f="791." m="79.9175" t="0.053"/>\r
+<eng-data cg="76." f="765." m="78.8979" t="0.056"/>\r
+<eng-data cg="76." f="755." m="77.9018" t="0.059"/>\r
+<eng-data cg="76." f="747." m="76.9176" t="0.062"/>\r
+<eng-data cg="76." f="737." m="74.6485" t="0.069"/>\r
+<eng-data cg="76." f="761." m="72.6852" t="0.075"/>\r
+<eng-data cg="76." f="755." m="70.3673" t="0.082"/>\r
+<eng-data cg="76." f="729." m="68.4223" t="0.088"/>\r
+<eng-data cg="76." f="741." m="66.8169" t="0.093"/>\r
+<eng-data cg="76." f="751." m="64.5356" t="0.1"/>\r
+<eng-data cg="76." f="703." m="32.7758" t="0.2"/>\r
+<eng-data cg="76." f="640." m="18.1081" t="0.25"/>\r
+<eng-data cg="76." f="586." m="4.71832" t="0.3"/>\r
+<eng-data cg="76." f="584." m="3.18494" t="0.306"/>\r
+<eng-data cg="76." f="576." m="2.4248" t="0.309"/>\r
+<eng-data cg="76." f="506." m="1.71577" t="0.312"/>\r
+<eng-data cg="76." f="292." m="0.669927" t="0.318"/>\r
+<eng-data cg="76." f="93." m="0.0812563" t="0.325"/>\r
+<eng-data cg="76." f="0." m="0." t="0.329"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech H70W\r
-; Copyright Tripoli Motor Testing 1997 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-H70W 29 229 0 0.11648 0.224 AT\r
- 0.055 114.847\r
- 0.169 131.427\r
- 0.283 126.879\r
- 0.397 127.136\r
- 0.510 127.254\r
- 0.625 125.894\r
- 0.739 124.917\r
- 0.852 122.031\r
- 0.967 119.032\r
- 1.080 115.071\r
- 1.194 108.446\r
- 1.308 102.273\r
- 1.422 96.098\r
- 1.535 86.953\r
- 1.650 75.702\r
- 1.764 62.402\r
- 1.877 48.132\r
- 1.992 36.862\r
- 2.105 28.065\r
- 2.219 21.592\r
- 2.333 16.894\r
- 2.447 12.686\r
- 2.560 9.681\r
- 2.675 6.818\r
- 2.790 4.488\r
- 2.904 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="199." Itot="200.23" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="70.01" burn-time="2.86" cgDiv="10" cgFix="1" cgStep="-1." code="H70W" delays="6,10,14" dia="29." exitDia="0." initWt="172." len="197." mDiv="10" mFix="1" mStep="-1." massFrac="59.65" mfg="Aerotech" peakThrust="107." propWt="102.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="98.5" f="0." m="102.6" t="0."/>\r
+<eng-data cg="98.5" f="107." m="99.8586" t="0.1"/>\r
+<eng-data cg="98.5" f="75." m="57.8922" t="1."/>\r
+<eng-data cg="98.5" f="61." m="5.62627" t="2.5"/>\r
+<eng-data cg="98.5" f="0." m="0." t="2.86"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech H73J\r
-; Copyright Tripoli Motor Testing 1997 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-H73J 38 152 6 0.14784 0.30912 AT\r
- 0.056 49.252\r
- 0.172 82.004\r
- 0.287 82.130\r
- 0.403 84.596\r
- 0.520 86.883\r
- 0.635 88.888\r
- 0.751 89.652\r
- 0.867 91.342\r
- 0.982 92.980\r
- 1.099 94.571\r
- 1.215 94.641\r
- 1.330 93.549\r
- 1.446 91.447\r
- 1.561 88.189\r
- 1.678 82.436\r
- 1.794 77.397\r
- 1.909 70.772\r
- 2.025 61.173\r
- 2.141 51.161\r
- 2.257 38.540\r
- 2.373 21.562\r
- 2.489 12.213\r
- 2.604 7.327\r
- 2.720 3.706\r
- 2.836 1.777\r
- 2.953 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="131.14" Itot="180.052" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="51.443" burn-time="3.5" cgDiv="10" cgFix="1" cgStep="-1." code="H73J" delays="6,10" dia="38." exitDia="0." initWt="308.3" len="154." mDiv="10" mFix="1" mStep="-1." massFrac="45.41" mfg="Aerotech" peakThrust="69.57" propWt="140." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="77." f="0." m="140." t="0."/>\r
+<eng-data cg="77." f="69.57" m="140." t="0."/>\r
+<eng-data cg="77." f="61.43" m="114.535" t="0.5"/>\r
+<eng-data cg="77." f="57.38" m="68.3444" t="1.5"/>\r
+<eng-data cg="77." f="57.38" m="37.1131" t="2.2"/>\r
+<eng-data cg="77." f="49.15" m="20.5465" t="2.6"/>\r
+<eng-data cg="77." f="45.06" m="16.8838" t="2.7"/>\r
+<eng-data cg="77." f="36.87" m="10.5133" t="2.9"/>\r
+<eng-data cg="77." f="32.78" m="5.09765" t="3.1"/>\r
+<eng-data cg="77." f="28.69" m="2.70784" t="3.2"/>\r
+<eng-data cg="77." f="4.09" m="0.15901" t="3.4"/>\r
+<eng-data cg="77." f="0." m="0." t="3.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech H97J\r
-; Copyright Tripoli Motor Testing 1997 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-H97J 29 238 6 0.1344 0.27776 AT\r
- 0.045 89.405\r
- 0.136 100.289\r
- 0.228 100.463\r
- 0.320 102.019\r
- 0.411 102.813\r
- 0.503 103.550\r
- 0.595 101.701\r
- 0.686 103.056\r
- 0.778 103.331\r
- 0.870 102.613\r
- 0.961 103.394\r
- 1.053 100.963\r
- 1.145 101.226\r
- 1.236 99.864\r
- 1.328 98.420\r
- 1.420 96.827\r
- 1.511 95.034\r
- 1.603 93.241\r
- 1.695 93.485\r
- 1.786 88.068\r
- 1.878 64.358\r
- 1.970 30.264\r
- 2.061 8.691\r
- 2.153 1.399\r
- 2.245 0.525\r
- 2.336 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="134.07" Itot="185.248" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="115.78" burn-time="1.6" cgDiv="10" cgFix="1" cgStep="-1." code="H97J" delays="6,10" dia="29." exitDia="0." initWt="281.5" len="239." mDiv="10" mFix="1" mStep="-1." massFrac="50.05" mfg="Aerotech" peakThrust="127.92" propWt="140.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="119.5" f="0." m="140.9" t="0."/>\r
+<eng-data cg="119.5" f="117.56" m="140.9" t="0."/>\r
+<eng-data cg="119.5" f="111.24" m="132.199" t="0.1"/>\r
+<eng-data cg="119.5" f="111.24" m="123.738" t="0.2"/>\r
+<eng-data cg="119.5" f="111.24" m="115.277" t="0.3"/>\r
+<eng-data cg="119.5" f="116.8" m="106.604" t="0.4"/>\r
+<eng-data cg="119.5" f="127.92" m="97.2977" t="0.5"/>\r
+<eng-data cg="119.5" f="116.8" m="87.991" t="0.6"/>\r
+<eng-data cg="119.5" f="122.36" m="78.8957" t="0.7"/>\r
+<eng-data cg="119.5" f="127.92" m="40.823" t="1.1"/>\r
+<eng-data cg="119.5" f="116.8" m="22.2096" t="1.3"/>\r
+<eng-data cg="119.5" f="116.8" m="4.44192" t="1.5"/>\r
+<eng-data cg="119.5" f="0." m="0." t="1.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; 38-360\r
-; Greg Gardner - 09/15/06\r
-H999N 38 203 0 0.144 0.331 AT\r
-0.003 204\r
-0.006 757\r
-0.009 1357\r
-0.012 1710\r
-0.016 1345\r
-0.019 995\r
-0.022 710\r
-0.025 606\r
-0.028 905\r
-0.031 1165\r
-0.0325 1311\r
-0.034 1258\r
-0.037 1098\r
-0.04 1072\r
-0.043 969\r
-0.047 1072\r
-0.0485 1166\r
-0.05 1098\r
-0.053 1160\r
-0.056 1117\r
-0.059 1103\r
-0.062 1093\r
-0.069 1076\r
-0.075 1110\r
-0.082 1105\r
-0.088 1065\r
-0.093 1082\r
-0.1 1092\r
-0.2 1022\r
-0.25 931\r
-0.3 853\r
-0.306 850\r
-0.309 838\r
-0.312 735\r
-0.318 435\r
-0.325 161\r
-0.329 0\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="226.6" Itot="319.993" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="972.624" burn-time="0.33" cgDiv="10" cgFix="1" cgStep="-1." code="H999N" delays="1000" dia="38." exitDia="0." initWt="331." len="203." mDiv="10" mFix="1" mStep="-1." massFrac="43.5" mfg="Aerotech" peakThrust="1710." propWt="144." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Greg Gardner - 09/15/06</comments>\r
+<data>\r
+<eng-data cg="101.5" f="0." m="144." t="0."/>\r
+<eng-data cg="101.5" f="204." m="143.862" t="0.003"/>\r
+<eng-data cg="101.5" f="757." m="143.214" t="0.006"/>\r
+<eng-data cg="101.5" f="1357." m="141.787" t="0.009"/>\r
+<eng-data cg="101.5" f="1710." m="139.716" t="0.012"/>\r
+<eng-data cg="101.5" f="1345." m="136.967" t="0.016"/>\r
+<eng-data cg="101.5" f="995." m="135.387" t="0.019"/>\r
+<eng-data cg="101.5" f="710." m="134.236" t="0.022"/>\r
+<eng-data cg="101.5" f="606." m="133.348" t="0.025"/>\r
+<eng-data cg="101.5" f="905." m="132.328" t="0.028"/>\r
+<eng-data cg="101.5" f="1165." m="130.931" t="0.031"/>\r
+<eng-data cg="101.5" f="1311." m="130.095" t="0.0325"/>\r
+<eng-data cg="101.5" f="1258." m="129.228" t="0.034"/>\r
+<eng-data cg="101.5" f="1098." m="127.638" t="0.037"/>\r
+<eng-data cg="101.5" f="1072." m="126.173" t="0.04"/>\r
+<eng-data cg="101.5" f="969." m="124.795" t="0.043"/>\r
+<eng-data cg="101.5" f="1072." m="122.958" t="0.047"/>\r
+<eng-data cg="101.5" f="1166." m="122.203" t="0.0485"/>\r
+<eng-data cg="101.5" f="1098." m="121.439" t="0.05"/>\r
+<eng-data cg="101.5" f="1160." m="119.915" t="0.053"/>\r
+<eng-data cg="101.5" f="1117." m="118.378" t="0.056"/>\r
+<eng-data cg="101.5" f="1103." m="116.879" t="0.059"/>\r
+<eng-data cg="101.5" f="1093." m="115.397" t="0.062"/>\r
+<eng-data cg="101.5" f="1076." m="111.981" t="0.069"/>\r
+<eng-data cg="101.5" f="1110." m="109.029" t="0.075"/>\r
+<eng-data cg="101.5" f="1105." m="105.541" t="0.082"/>\r
+<eng-data cg="101.5" f="1065." m="102.611" t="0.088"/>\r
+<eng-data cg="101.5" f="1082." m="100.196" t="0.093"/>\r
+<eng-data cg="101.5" f="1092." m="96.7716" t="0.1"/>\r
+<eng-data cg="101.5" f="1022." m="49.2056" t="0.2"/>\r
+<eng-data cg="101.5" f="931." m="27.2339" t="0.25"/>\r
+<eng-data cg="101.5" f="853." m="7.16348" t="0.3"/>\r
+<eng-data cg="101.5" f="850." m="4.86438" t="0.306"/>\r
+<eng-data cg="101.5" f="838." m="3.72495" t="0.309"/>\r
+<eng-data cg="101.5" f="735." m="2.66316" t="0.312"/>\r
+<eng-data cg="101.5" f="435." m="1.08362" t="0.318"/>\r
+<eng-data cg="101.5" f="161." m="0.144903" t="0.325"/>\r
+<eng-data cg="101.5" f="0." m="0." t="0.329"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;Entered by Jim Yehle\r
-;from TRA cert document\r
-I1299N 38 249 1000 0.192 0.422 AT-RMS \r
-0 15.7171\r
-0.00361 222.5\r
-0.0115 1112\r
-0.0134228 1237.11\r
-0.02 1287\r
-0.04 1359\r
-0.1 1451\r
-0.12 1470\r
-0.18 1491\r
-0.2 1483\r
-0.22 1462\r
-0.24 1399\r
-0.28 1208\r
-0.294743 1131.63\r
-0.3 1065\r
-0.304251 974.46\r
-0.32 305\r
-0.330537 55.0098\r
-0.333893 11.7878\r
-0.34 0\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="AT-RMS" code="I1299N" Type="reloadable" dia="38." len="249." initWt="422."\r
+propWt="192." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="1248.44" peakThrust="1491." throatDia="0." exitDia="0." Itot="424.469"\r
+burn-time="0.34" massFrac="45.5" Isp="225.44" tDiv="10" tStep="-1." tFix="1"\r
+FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+ <comments>Entered by Jim Yehle\r
+from TRA cert document\r
+</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="192." cg="124.5"/>\r
+ <eng-data t="0." f="15.7171" m="192." cg="124.5"/>\r
+ <eng-data t="0.00361" f="222.5" m="191.806" cg="124.5"/>\r
+ <eng-data t="0.0115" f="1112." m="189.424" cg="124.5"/>\r
+ <eng-data t="0.0134228" f="1237.11" m="188.403" cg="124.5"/>\r
+ <eng-data t="0.02" f="1287." m="184.648" cg="124.5"/>\r
+ <eng-data t="0.04" f="1359." m="172.679" cg="124.5"/>\r
+ <eng-data t="0.1" f="1451." m="134.548" cg="124.5"/>\r
+ <eng-data t="0.12" f="1470." m="121.335" cg="124.5"/>\r
+ <eng-data t="0.18" f="1491." m="81.1548" cg="124.5"/>\r
+ <eng-data t="0.2" f="1483." m="67.7025" cg="124.5"/>\r
+ <eng-data t="0.22" f="1462." m="54.3814" cg="124.5"/>\r
+ <eng-data t="0.24" f="1399." m="41.4402" cg="124.5"/>\r
+ <eng-data t="0.28" f="1208." m="17.8557" cg="124.5"/>\r
+ <eng-data t="0.294743" f="1131.63" m="10.0547" cg="124.5"/>\r
+ <eng-data t="0.3" f="1065." m="7.4429" cg="124.5"/>\r
+ <eng-data t="0.304251" f="974.46" m="5.48231" cg="124.5"/>\r
+ <eng-data t="0.32" f="305." m="0.92491" cg="124.5"/>\r
+ <eng-data t="0.330537" f="55.0098" m="0.0669778" cg="124.5"/>\r
+ <eng-data t="0.333893" f="11.7878" m="0.0162822" cg="124.5"/>\r
+ <eng-data t="0.34" f="0." m="0." cg="124.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech I132W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I132W 38 335 0 0.365568 0.512064 AT\r
- 0.096 204.011\r
- 0.290 174.236\r
- 0.484 168.865\r
- 0.679 170.783\r
- 0.874 173.028\r
- 1.069 174.287\r
- 1.264 174.647\r
- 1.458 174.364\r
- 1.652 174.645\r
- 1.847 173.002\r
- 2.042 169.209\r
- 2.236 164.309\r
- 2.431 157.149\r
- 2.626 149.580\r
- 2.821 138.360\r
- 3.016 124.171\r
- 3.210 107.626\r
- 3.404 89.785\r
- 3.599 71.747\r
- 3.794 55.124\r
- 3.989 42.264\r
- 4.183 31.373\r
- 4.378 21.980\r
- 4.573 14.389\r
- 4.768 8.794\r
- 4.962 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="201.17" Itot="639.965" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="131.952" burn-time="4.85" cgDiv="10" cgFix="1" cgStep="-1." code="I132W" delays="10,14" dia="38." exitDia="0." initWt="557." len="330." mDiv="10" mFix="1" mStep="-1." massFrac="58.24" mfg="Aerotech" peakThrust="227." propWt="324.4" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="165." f="0." m="324.4" t="0."/>\r
+<eng-data cg="165." f="89." m="323.047" t="0.06"/>\r
+<eng-data cg="165." f="227." m="207.716" t="1.5"/>\r
+<eng-data cg="165." f="143." m="67.0506" t="3."/>\r
+<eng-data cg="165." f="0." m="0." t="4.85"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech I154J\r
-; Copyright Tripoli Motor Testing 1999 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I154J 38 250 0 0.25088 0.491904 AT\r
- 0.066 120.409\r
- 0.199 150.638\r
- 0.332 151.666\r
- 0.466 156.806\r
- 0.599 150.331\r
- 0.732 150.602\r
- 0.866 145.101\r
- 0.999 144.469\r
- 1.133 145.159\r
- 1.268 145.912\r
- 1.401 141.710\r
- 1.534 142.828\r
- 1.668 141.187\r
- 1.801 140.970\r
- 1.934 137.832\r
- 2.068 128.417\r
- 2.202 122.339\r
- 2.336 111.986\r
- 2.470 105.295\r
- 2.603 96.602\r
- 2.736 90.469\r
- 2.870 57.427\r
- 3.003 20.489\r
- 3.136 4.707\r
- 3.271 2.966\r
- 3.405 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="140.33" Itot="385.327" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="107.035" burn-time="3.6" cgDiv="10" cgFix="1" cgStep="-1." code="I154J" delays="6,10" dia="38." exitDia="0." initWt="506.3" len="250." mDiv="10" mFix="1" mStep="-1." massFrac="55.3" mfg="Aerotech" peakThrust="199.49" propWt="280." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="125." f="0." m="280." t="0."/>\r
+<eng-data cg="125." f="199.49" m="280." t="0."/>\r
+<eng-data cg="125." f="162.84" m="266.836" t="0.1"/>\r
+<eng-data cg="125." f="153.9" m="243.819" t="0.3"/>\r
+<eng-data cg="125." f="149.32" m="232.803" t="0.4"/>\r
+<eng-data cg="125." f="149.32" m="211.102" t="0.6"/>\r
+<eng-data cg="125." f="126.72" m="170.985" t="1."/>\r
+<eng-data cg="125." f="117.65" m="117.713" t="1.6"/>\r
+<eng-data cg="125." f="113.11" m="109.329" t="1.7"/>\r
+<eng-data cg="125." f="113.11" m="76.4518" t="2.1"/>\r
+<eng-data cg="125." f="95.05" m="38.6366" t="2.6"/>\r
+<eng-data cg="125." f="67.88" m="9.03814" t="3.1"/>\r
+<eng-data cg="125." f="22.6" m="2.46336" t="3.3"/>\r
+<eng-data cg="125." f="0." m="0." t="3.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech I161W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I161W 38 191 0 0.189952 0.370048 AT\r
- 0.043 178.900\r
- 0.131 206.770\r
- 0.221 206.101\r
- 0.310 205.175\r
- 0.400 206.924\r
- 0.490 210.603\r
- 0.579 210.475\r
- 0.669 211.555\r
- 0.758 212.379\r
- 0.848 212.096\r
- 0.938 209.060\r
- 1.027 202.345\r
- 1.116 192.439\r
- 1.204 179.499\r
- 1.294 162.159\r
- 1.383 148.446\r
- 1.473 135.222\r
- 1.563 120.095\r
- 1.652 104.041\r
- 1.742 87.962\r
- 1.831 74.789\r
- 1.921 54.362\r
- 2.010 23.386\r
- 2.100 7.332\r
- 2.190 5.171\r
- 2.279 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="181.38" Itot="333.514" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="145.006" burn-time="2.3" cgDiv="10" cgFix="1" cgStep="-1." code="I161W" delays="6,10,14" dia="38." exitDia="0." initWt="384.8" len="202." mDiv="10" mFix="1" mStep="-1." massFrac="48.73" mfg="Aerotech" peakThrust="224.89" propWt="187.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="101." f="0." m="187.5" t="0."/>\r
+<eng-data cg="101." f="0.09" m="187.5" t="0."/>\r
+<eng-data cg="101." f="224.89" m="181.176" t="0.1"/>\r
+<eng-data cg="101." f="206.88" m="169.039" t="0.2"/>\r
+<eng-data cg="101." f="202.43" m="134.522" t="0.5"/>\r
+<eng-data cg="101." f="184.41" m="112.774" t="0.7"/>\r
+<eng-data cg="101." f="179.92" m="82.0506" t="1."/>\r
+<eng-data cg="101." f="166.4" m="52.8457" t="1.3"/>\r
+<eng-data cg="101." f="134.91" m="27.4365" t="1.6"/>\r
+<eng-data cg="101." f="112.44" m="13.5306" t="1.8"/>\r
+<eng-data cg="101." f="62.98" m="3.6686" t="2."/>\r
+<eng-data cg="101." f="22.51" m="1.2655" t="2.1"/>\r
+<eng-data cg="101." f="0." m="0." t="2.3"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech I195J\r
-; Copyright Tripoli Motor Testing 1996 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I195J 38 298 10 0.3136 0.59136 AT\r
- 0.050 258.670\r
- 0.152 353.638\r
- 0.254 300.655\r
- 0.356 265.354\r
- 0.458 266.338\r
- 0.560 283.233\r
- 0.662 332.442\r
- 0.765 283.040\r
- 0.867 230.795\r
- 0.969 222.867\r
- 1.071 217.091\r
- 1.173 210.600\r
- 1.275 202.722\r
- 1.377 192.671\r
- 1.479 182.571\r
- 1.581 171.964\r
- 1.683 162.238\r
- 1.785 148.138\r
- 1.888 130.259\r
- 1.990 107.022\r
- 2.092 80.230\r
- 2.194 51.074\r
- 2.296 26.313\r
- 2.398 10.397\r
- 2.500 3.977\r
- 2.602 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="148.54" Itot="455.2" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="160.848" burn-time="2.83" cgDiv="10" cgFix="1" cgStep="-1." code="I195J" delays="6,10,14" dia="38." exitDia="0." initWt="582.4" len="297." mDiv="10" mFix="1" mStep="-1." massFrac="53.66" mfg="Aerotech" peakThrust="244.78" propWt="312.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="148.5" f="0." m="312.5" t="0."/>\r
+<eng-data cg="148.5" f="244.78" m="312.5" t="0."/>\r
+<eng-data cg="148.5" f="236.61" m="295.976" t="0.1"/>\r
+<eng-data cg="148.5" f="216.19" m="280.433" t="0.2"/>\r
+<eng-data cg="148.5" f="212.11" m="265.732" t="0.3"/>\r
+<eng-data cg="148.5" f="212.11" m="105.554" t="1.4"/>\r
+<eng-data cg="148.5" f="203.94" m="91.2728" t="1.5"/>\r
+<eng-data cg="148.5" f="188.46" m="77.8035" t="1.6"/>\r
+<eng-data cg="148.5" f="179.49" m="65.1734" t="1.7"/>\r
+<eng-data cg="148.5" f="156.65" m="53.6352" t="1.8"/>\r
+<eng-data cg="148.5" f="142.78" m="43.357" t="1.9"/>\r
+<eng-data cg="148.5" f="130.53" m="33.9755" t="2."/>\r
+<eng-data cg="148.5" f="118.28" m="25.435" t="2.1"/>\r
+<eng-data cg="148.5" f="106.08" m="17.7337" t="2.2"/>\r
+<eng-data cg="148.5" f="89.74" m="11.012" t="2.3"/>\r
+<eng-data cg="148.5" f="63.63" m="5.74751" t="2.4"/>\r
+<eng-data cg="148.5" f="32.62" m="2.44367" t="2.5"/>\r
+<eng-data cg="148.5" f="8.97" m="1.01607" t="2.6"/>\r
+<eng-data cg="148.5" f="8.97" m="0.400271" t="2.7"/>\r
+<eng-data cg="148.5" f="0." m="0." t="2.83"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech I195J\r
-; Copyright Tripoli Motor Testing 1999 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I195J 38 297 0 0.296576 0.563136 AT\r
- 0.033 190.099\r
- 0.103 354.046\r
- 0.173 393.473\r
- 0.243 414.842\r
- 0.314 379.747\r
- 0.383 364.640\r
- 0.453 364.776\r
- 0.524 357.242\r
- 0.594 355.802\r
- 0.664 355.644\r
- 0.734 353.557\r
- 0.804 339.941\r
- 0.874 309.753\r
- 0.944 275.017\r
- 1.014 243.739\r
- 1.084 218.135\r
- 1.154 197.291\r
- 1.224 173.680\r
- 1.295 147.000\r
- 1.365 116.506\r
- 1.434 83.105\r
- 1.505 51.011\r
- 1.575 26.480\r
- 1.645 13.927\r
- 1.716 7.273\r
- 1.786 0.000\r
+++ /dev/null
-; AeroTech I200W\r
-; Copyright Tripoli Motor Testing 1999 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I200W 29 333 0 0.181888 0.357504 AT\r
- 0.033 303.951\r
- 0.103 273.452\r
- 0.174 276.061\r
- 0.245 271.625\r
- 0.316 268.233\r
- 0.386 258.449\r
- 0.457 252.480\r
- 0.528 246.642\r
- 0.599 242.304\r
- 0.670 237.737\r
- 0.741 234.769\r
- 0.811 233.171\r
- 0.882 230.660\r
- 0.953 224.985\r
- 1.024 221.658\r
- 1.095 214.548\r
- 1.166 177.365\r
- 1.236 154.208\r
- 1.307 119.146\r
- 1.378 91.586\r
- 1.449 65.330\r
- 1.520 32.877\r
- 1.591 28.702\r
- 1.661 22.211\r
- 1.732 15.558\r
- 1.803 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="183.2" Itot="326.785" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="181.245" burn-time="1.8" cgDiv="10" cgFix="1" cgStep="-1." code="I200W" delays="6,10,14" dia="29." exitDia="0." initWt="357.504" len="333." mDiv="10" mFix="1" mStep="-1." massFrac="50.88" mfg="Aerotech" peakThrust="303.951" propWt="181.888" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="166.5" f="0." m="181.888" t="0."/>\r
+<eng-data cg="166.5" f="303.951" m="179.097" t="0.033"/>\r
+<eng-data cg="166.5" f="273.452" m="167.848" t="0.103"/>\r
+<eng-data cg="166.5" f="276.061" m="156.99" t="0.174"/>\r
+<eng-data cg="166.5" f="271.625" m="146.168" t="0.245"/>\r
+<eng-data cg="166.5" f="268.233" m="135.501" t="0.316"/>\r
+<eng-data cg="166.5" f="258.449" m="125.241" t="0.386"/>\r
+<eng-data cg="166.5" f="252.48" m="115.145" t="0.457"/>\r
+<eng-data cg="166.5" f="246.642" m="105.283" t="0.528"/>\r
+<eng-data cg="166.5" f="242.304" m="95.6219" t="0.599"/>\r
+<eng-data cg="166.5" f="237.737" m="86.1366" t="0.67"/>\r
+<eng-data cg="166.5" f="234.769" m="76.8003" t="0.741"/>\r
+<eng-data cg="166.5" f="233.171" m="67.6843" t="0.811"/>\r
+<eng-data cg="166.5" f="230.66" m="58.5194" t="0.882"/>\r
+<eng-data cg="166.5" f="224.985" m="49.5162" t="0.953"/>\r
+<eng-data cg="166.5" f="221.658" m="40.6909" t="1.024"/>\r
+<eng-data cg="166.5" f="214.548" m="32.0718" t="1.095"/>\r
+<eng-data cg="166.5" f="177.365" m="24.3279" t="1.166"/>\r
+<eng-data cg="166.5" f="154.208" m="17.8685" t="1.236"/>\r
+<eng-data cg="166.5" f="119.146" m="12.4672" t="1.307"/>\r
+<eng-data cg="166.5" f="91.586" m="8.30333" t="1.378"/>\r
+<eng-data cg="166.5" f="65.33" m="5.20279" t="1.449"/>\r
+<eng-data cg="166.5" f="32.877" m="3.26229" t="1.52"/>\r
+<eng-data cg="166.5" f="28.702" m="2.04553" t="1.591"/>\r
+<eng-data cg="166.5" f="22.211" m="1.0537" t="1.661"/>\r
+<eng-data cg="166.5" f="15.558" m="0.307414" t="1.732"/>\r
+<eng-data cg="166.5" f="0." m="0." t="1.803"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech I211W\r
-; Copyright Tripoli Motor Testing 1999 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I211W 38 240 0 0.247296 0.466368 AT\r
- 0.044 257.326\r
- 0.134 295.533\r
- 0.226 296.087\r
- 0.318 298.204\r
- 0.408 295.082\r
- 0.499 287.669\r
- 0.591 282.578\r
- 0.682 272.875\r
- 0.773 266.997\r
- 0.864 257.602\r
- 0.955 250.495\r
- 1.047 238.574\r
- 1.138 228.571\r
- 1.228 215.135\r
- 1.320 198.047\r
- 1.411 180.631\r
- 1.502 161.261\r
- 1.593 146.708\r
- 1.684 134.484\r
- 1.776 101.241\r
- 1.867 52.688\r
- 1.957 35.461\r
- 2.049 24.321\r
- 2.141 11.165\r
- 2.232 4.587\r
- 2.324 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="179.66" Itot="440.462" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="200.21" burn-time="2.2" cgDiv="10" cgFix="1" cgStep="-1." code="I211W" delays="6,10,14" dia="38." exitDia="0." initWt="476.3" len="250." mDiv="10" mFix="1" mStep="-1." massFrac="52.49" mfg="Aerotech" peakThrust="386." propWt="250." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="125." f="0." m="250." t="0."/>\r
+<eng-data cg="125." f="386." m="250." t="0."/>\r
+<eng-data cg="125." f="289.39" m="230.833" t="0.1"/>\r
+<eng-data cg="125." f="276.22" m="214.781" t="0.2"/>\r
+<eng-data cg="125." f="276.22" m="199.103" t="0.3"/>\r
+<eng-data cg="125." f="293.79" m="182.927" t="0.4"/>\r
+<eng-data cg="125." f="271.86" m="166.874" t="0.5"/>\r
+<eng-data cg="125." f="271.86" m="151.444" t="0.6"/>\r
+<eng-data cg="125." f="206.08" m="56.4989" t="1.3"/>\r
+<eng-data cg="125." f="131.57" m="8.58756" t="1.8"/>\r
+<eng-data cg="125." f="52.62" m="3.36039" t="1.9"/>\r
+<eng-data cg="125." f="21.93" m="1.24471" t="2."/>\r
+<eng-data cg="125." f="0." m="0." t="2.2"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech I218R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I218R 38 191 0 0.19264 0.37184 AT\r
- 0.027 136.078\r
- 0.088 275.030\r
- 0.148 280.998\r
- 0.208 284.371\r
- 0.268 284.037\r
- 0.327 279.311\r
- 0.388 277.791\r
- 0.448 276.309\r
- 0.509 269.384\r
- 0.570 266.041\r
- 0.630 261.907\r
- 0.690 256.366\r
- 0.750 250.565\r
- 0.810 242.206\r
- 0.870 234.607\r
- 0.930 225.488\r
- 0.991 216.166\r
- 1.053 205.415\r
- 1.112 193.238\r
- 1.173 177.206\r
- 1.233 161.304\r
- 1.292 139.118\r
- 1.353 96.082\r
- 1.413 38.848\r
- 1.474 5.978\r
- 1.535 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="168.84" Itot="317.901" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="211.934" burn-time="1.5" cgDiv="10" cgFix="1" cgStep="-1." code="I218R" delays="6,14,1000" dia="38." exitDia="0." initWt="375." len="191." mDiv="10" mFix="1" mStep="-1." massFrac="51.2" mfg="Aerotech" peakThrust="284.37" propWt="192." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="95.5" f="0." m="192." t="0."/>\r
+<eng-data cg="95.5" f="136.08" m="190.767" t="0.03"/>\r
+<eng-data cg="95.5" f="275.03" m="183.318" t="0.09"/>\r
+<eng-data cg="95.5" f="281." m="173.244" t="0.15"/>\r
+<eng-data cg="95.5" f="284.37" m="163." t="0.21"/>\r
+<eng-data cg="95.5" f="284.04" m="152.701" t="0.27"/>\r
+<eng-data cg="95.5" f="279.31" m="142.494" t="0.33"/>\r
+<eng-data cg="95.5" f="277.79" m="132.4" t="0.39"/>\r
+<eng-data cg="95.5" f="276.31" m="122.36" t="0.45"/>\r
+<eng-data cg="95.5" f="269.38" m="112.473" t="0.51"/>\r
+<eng-data cg="95.5" f="266.04" m="102.772" t="0.57"/>\r
+<eng-data cg="95.5" f="261.91" m="93.2058" t="0.63"/>\r
+<eng-data cg="95.5" f="256.37" m="83.8152" t="0.69"/>\r
+<eng-data cg="95.5" f="250.57" m="74.63" t="0.75"/>\r
+<eng-data cg="95.5" f="242.21" m="65.7014" t="0.81"/>\r
+<eng-data cg="95.5" f="234.61" m="57.062" t="0.87"/>\r
+<eng-data cg="95.5" f="225.49" m="48.7255" t="0.93"/>\r
+<eng-data cg="95.5" f="216.17" m="40.7232" t="0.99"/>\r
+<eng-data cg="95.5" f="205.41" m="33.0846" t="1.05"/>\r
+<eng-data cg="95.5" f="193.24" m="25.8616" t="1.11"/>\r
+<eng-data cg="95.5" f="177.21" m="19.1494" t="1.17"/>\r
+<eng-data cg="95.5" f="161.3" m="13.016" t="1.23"/>\r
+<eng-data cg="95.5" f="139.12" m="7.57277" t="1.29"/>\r
+<eng-data cg="95.5" f="96.08" m="3.31122" t="1.35"/>\r
+<eng-data cg="95.5" f="38.85" m="0.866443" t="1.41"/>\r
+<eng-data cg="95.5" f="5.98" m="0.0541753" t="1.47"/>\r
+<eng-data cg="95.5" f="0." m="0." t="1.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;Ejection delays may not be corrrect.\r
-;From Aerotech pre-cert data.\r
-;Created 11/11/07 by Jim Yehle.\r
-I245G 38 192.532 0-6-10-14 0.1813 0.365 Aerotech \r
-0.0244989 234.061\r
-0.0550162 257.888\r
-0.0868597 368.567\r
-0.106904 382.335\r
-0.13363 390.808\r
-0.200445 405.635\r
-0.262806 410.931\r
-0.302895 411.99\r
-0.363029 408.813\r
-0.401294 398.43\r
-0.501114 363.271\r
-0.594655 320.907\r
-0.68932 278.355\r
-0.797327 212.879\r
-0.893204 181.477\r
-1.00647 154.187\r
-1.09061 133.72\r
-1.16036 120.737\r
-1.1804 122.856\r
-1.23625 106.43\r
-1.30421 75.0467\r
-1.3608 36.0094\r
-1.40312 19.0638\r
-1.43875 5.2955\r
-1.46325 0\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Aerotech" code="I245G" Type="reloadable" dia="38." len="192.532"\r
+initWt="365." propWt="181.3" delays="0,6,10,14" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="239.565" peakThrust="411.99" throatDia="0."\r
+exitDia="0." Itot="350.544" burn-time="1.46" massFrac="49.67" Isp="197.16"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Ejection delays may not be corrrect.\r
+From Aerotech pre-cert data.\r
+Created 11/11/07 by Jim Yehle.</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="181.3" cg="96.266"/>\r
+ <eng-data t="0.0244989" f="234.061" m="179.817" cg="96.266"/>\r
+ <eng-data t="0.0550162" f="257.888" m="175.935" cg="96.266"/>\r
+ <eng-data t="0.0868597" f="368.567" m="170.776" cg="96.266"/>\r
+ <eng-data t="0.106904" f="382.335" m="166.884" cg="96.266"/>\r
+ <eng-data t="0.13363" f="390.808" m="161.54" cg="96.266"/>\r
+ <eng-data t="0.200445" f="405.635" m="147.779" cg="96.266"/>\r
+ <eng-data t="0.262806" f="410.931" m="134.611" cg="96.266"/>\r
+ <eng-data t="0.302895" f="411.99" m="126.08" cg="96.266"/>\r
+ <eng-data t="0.363029" f="408.813" m="113.316" cg="96.266"/>\r
+ <eng-data t="0.401294" f="398.43" m="105.328" cg="96.266"/>\r
+ <eng-data t="0.501114" f="363.271" m="85.6662" cg="96.266"/>\r
+ <eng-data t="0.594655" f="320.907" m="69.1163" cg="96.266"/>\r
+ <eng-data t="0.68932" f="278.355" m="54.4461" cg="96.266"/>\r
+ <eng-data t="0.797327" f="212.879" m="40.7258" cg="96.266"/>\r
+ <eng-data t="0.893204" f="181.477" m="30.9483" cg="96.266"/>\r
+ <eng-data t="1.00647" f="154.187" m="21.1164" cg="96.266"/>\r
+ <eng-data t="1.09061" f="133.72" m="14.8518" cg="96.266"/>\r
+ <eng-data t="1.16036" f="120.737" m="10.2627" cg="96.266"/>\r
+ <eng-data t="1.1804" f="122.856" m="9.00003" cg="96.266"/>\r
+ <eng-data t="1.23625" f="106.43" m="5.68882" cg="96.266"/>\r
+ <eng-data t="1.30421" f="75.0467" m="2.49944" cg="96.266"/>\r
+ <eng-data t="1.3608" f="36.0094" m="0.874102" cg="96.266"/>\r
+ <eng-data t="1.40312" f="19.0638" m="0.271441" cg="96.266"/>\r
+ <eng-data t="1.43875" f="5.2955" m="0.0469685" cg="96.266"/>\r
+ <eng-data t="1.46325" f="0" m="0." cg="96.266"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech I284W\r
-; Copyright Tripoli Motor Testing 1997 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I284W 38 298 10 0.3136 0.55552 AT\r
- 0.033 370.682\r
- 0.103 483.606\r
- 0.174 483.282\r
- 0.245 486.856\r
- 0.316 490.842\r
- 0.386 499.428\r
- 0.457 508.800\r
- 0.528 506.326\r
- 0.599 485.287\r
- 0.670 481.043\r
- 0.741 455.776\r
- 0.811 426.920\r
- 0.882 393.422\r
- 0.953 367.404\r
- 1.024 347.490\r
- 1.095 325.191\r
- 1.166 304.064\r
- 1.236 284.158\r
- 1.307 271.165\r
- 1.378 228.579\r
- 1.449 130.521\r
- 1.520 57.212\r
- 1.591 29.552\r
- 1.661 16.413\r
- 1.732 10.365\r
- 1.803 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="180.85" Itot="554.236" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="307.909" burn-time="1.8" cgDiv="10" cgFix="1" cgStep="-1." code="I284W" delays="6,10,14" dia="38." exitDia="0." initWt="567.8" len="297." mDiv="10" mFix="1" mStep="-1." massFrac="55.04" mfg="Aerotech" peakThrust="487.77" propWt="312.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="148.5" f="0." m="312.5" t="0."/>\r
+<eng-data cg="148.5" f="487.77" m="312.5" t="0."/>\r
+<eng-data cg="148.5" f="408.77" m="287.225" t="0.1"/>\r
+<eng-data cg="148.5" f="408.77" m="264.177" t="0.2"/>\r
+<eng-data cg="148.5" f="430.74" m="216.842" t="0.4"/>\r
+<eng-data cg="148.5" f="413.18" m="169.258" t="0.6"/>\r
+<eng-data cg="148.5" f="307.67" m="67.6475" t="1.1"/>\r
+<eng-data cg="148.5" f="250.51" m="36.1751" t="1.3"/>\r
+<eng-data cg="148.5" f="193.35" m="11.1485" t="1.5"/>\r
+<eng-data cg="148.5" f="79.08" m="3.46818" t="1.6"/>\r
+<eng-data cg="148.5" f="21.97" m="0.619377" t="1.7"/>\r
+<eng-data cg="148.5" f="0." m="0." t="1.8"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech I284W\r
-; Copyright Tripoli Motor Testing 1999 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I284W 38 297 0 0.310016 0.555072 AT\r
- 0.041 422.031\r
- 0.125 448.597\r
- 0.210 459.029\r
- 0.295 451.940\r
- 0.379 439.556\r
- 0.465 427.370\r
- 0.549 407.558\r
- 0.633 399.734\r
- 0.719 380.049\r
- 0.803 368.042\r
- 0.887 352.020\r
- 0.973 342.102\r
- 1.057 325.767\r
- 1.142 306.936\r
- 1.227 292.029\r
- 1.311 267.283\r
- 1.396 251.784\r
- 1.481 227.534\r
- 1.566 210.504\r
- 1.650 168.299\r
- 1.735 110.789\r
- 1.820 71.036\r
- 1.904 32.505\r
- 1.990 17.537\r
- 2.075 7.317\r
- 2.160 0.000\r
+++ /dev/null
-; AeroTech I285R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I285R 38 250 0 0.25088 0.4928 AT\r
- 0.027 171.405\r
- 0.088 325.573\r
- 0.148 341.697\r
- 0.208 358.916\r
- 0.268 373.706\r
- 0.327 373.966\r
- 0.388 368.442\r
- 0.448 367.497\r
- 0.507 361.900\r
- 0.568 351.928\r
- 0.628 346.109\r
- 0.687 340.993\r
- 0.749 329.382\r
- 0.810 321.625\r
- 0.870 310.856\r
- 0.930 295.955\r
- 0.990 283.704\r
- 1.050 269.655\r
- 1.110 253.419\r
- 1.170 240.222\r
- 1.230 224.116\r
- 1.290 204.118\r
- 1.350 118.730\r
- 1.410 23.483\r
- 1.471 2.046\r
- 1.532 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="166.59" Itot="414.966" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="276.644" burn-time="1.5" cgDiv="10" cgFix="1" cgStep="-1." code="I285R" delays="10,14,1000" dia="38." exitDia="0." initWt="498." len="250." mDiv="10" mFix="1" mStep="-1." massFrac="51." mfg="Aerotech" peakThrust="373.97" propWt="254." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="125." f="0." m="254." t="0."/>\r
+<eng-data cg="125." f="171.41" m="252.426" t="0.03"/>\r
+<eng-data cg="125." f="325.57" m="243.3" t="0.09"/>\r
+<eng-data cg="125." f="341.7" m="231.047" t="0.15"/>\r
+<eng-data cg="125." f="358.92" m="218.182" t="0.21"/>\r
+<eng-data cg="125." f="373.71" m="204.728" t="0.27"/>\r
+<eng-data cg="125." f="373.97" m="190.999" t="0.33"/>\r
+<eng-data cg="125." f="368.44" m="177.366" t="0.39"/>\r
+<eng-data cg="125." f="367.5" m="163.852" t="0.45"/>\r
+<eng-data cg="125." f="361.9" m="150.458" t="0.51"/>\r
+<eng-data cg="125." f="351.93" m="137.35" t="0.57"/>\r
+<eng-data cg="125." f="346.11" m="124.532" t="0.63"/>\r
+<eng-data cg="125." f="340.99" m="111.915" t="0.69"/>\r
+<eng-data cg="125." f="329.38" m="99.6047" t="0.75"/>\r
+<eng-data cg="125." f="321.63" m="87.6502" t="0.81"/>\r
+<eng-data cg="125." f="310.86" m="76.0358" t="0.87"/>\r
+<eng-data cg="125." f="295.95" m="64.893" t="0.93"/>\r
+<eng-data cg="125." f="283.7" m="54.2489" t="0.99"/>\r
+<eng-data cg="125." f="269.65" m="44.0877" t="1.05"/>\r
+<eng-data cg="125." f="253.42" m="34.4826" t="1.11"/>\r
+<eng-data cg="125." f="240.22" m="25.4179" t="1.17"/>\r
+<eng-data cg="125." f="224.12" m="16.8913" t="1.23"/>\r
+<eng-data cg="125." f="204.12" m="9.02751" t="1.29"/>\r
+<eng-data cg="125." f="118.73" m="3.09903" t="1.35"/>\r
+<eng-data cg="125." f="23.48" m="0.487628" t="1.41"/>\r
+<eng-data cg="125." f="2.05" m="0.018822" t="1.47"/>\r
+<eng-data cg="125." f="0." m="0." t="1.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-I300T 38 250 6-10-14 0.2216 0.4405 AT\r
-0 473.17\r
-0.1 395.68\r
-0.2 375.31\r
-0.3 367.14\r
-0.4 358.97\r
-0.5 346.72\r
-0.6 338.56\r
-0.7 318.19\r
-0.8 305.94\r
-0.9 295.35\r
-1.07 269.23\r
-1.1 258.01\r
-1.2 246.79\r
-1.3 179.49\r
-1.4 48.95\r
-1.5 13.91\r
-1.6 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="200.99" Itot="436.789" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="272.993" burn-time="1.6" cgDiv="10" cgFix="1" cgStep="-1." code="I300T" delays="6,10,14" dia="38." exitDia="0." initWt="440.5" len="250." mDiv="10" mFix="1" mStep="-1." massFrac="50.31" mfg="Aerotech" peakThrust="473.17" propWt="221.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="125." f="0." m="221.6" t="0."/>\r
+<eng-data cg="125." f="473.17" m="221.6" t="0."/>\r
+<eng-data cg="125." f="395.68" m="199.56" t="0.1"/>\r
+<eng-data cg="125." f="375.31" m="180.002" t="0.2"/>\r
+<eng-data cg="125." f="367.14" m="161.169" t="0.3"/>\r
+<eng-data cg="125." f="358.97" m="142.749" t="0.4"/>\r
+<eng-data cg="125." f="346.72" m="124.848" t="0.5"/>\r
+<eng-data cg="125." f="338.56" m="107.465" t="0.6"/>\r
+<eng-data cg="125." f="318.19" m="90.8051" t="0.7"/>\r
+<eng-data cg="125." f="305.94" m="74.9729" t="0.8"/>\r
+<eng-data cg="125." f="295.35" m="59.72" t="0.9"/>\r
+<eng-data cg="125." f="269.23" m="35.3732" t="1.07"/>\r
+<eng-data cg="125." f="258.01" m="31.3609" t="1.1"/>\r
+<eng-data cg="125." f="246.79" m="18.5556" t="1.2"/>\r
+<eng-data cg="125." f="179.49" m="7.74224" t="1.3"/>\r
+<eng-data cg="125." f="48.95" m="1.94742" t="1.4"/>\r
+<eng-data cg="125." f="13.91" m="0.352854" t="1.5"/>\r
+<eng-data cg="125." f="0." m="0." t="1.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; I305FJ based on Aerotech instruction sheet by C. Kobel 3/30/07\r
-I305FJ 38 298 6-10-14 0.302 0.581 AT\r
- 0.020 341.398\r
- 0.100 365.497\r
- 0.200 383.571\r
- 0.300 403.653\r
- 0.400 405.662\r
- 0.500 405.662\r
- 0.600 404.657\r
- 0.700 374.534\r
- 0.800 342.402\r
- 0.900 309.267\r
- 1.000 272.115\r
- 1.100 238.979\r
- 1.150 224.921\r
- 1.200 194.798\r
- 1.300 119.489\r
- 1.400 62.255\r
- 1.450 33.136\r
- 1.500 23.095\r
- 1.600 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="149.89" Itot="443.903" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="277.44" burn-time="1.6" cgDiv="10" cgFix="1" cgStep="-1." code="I305FJ" delays="6,10,14" dia="38." exitDia="0." initWt="581." len="298." mDiv="10" mFix="1" mStep="-1." massFrac="51.98" mfg="Aerotech" peakThrust="405.662" propWt="302." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>I305FJ based on Aerotech instruction sheet by C. Kobel 3/30/07</comments>\r
+<data>\r
+<eng-data cg="149." f="0." m="302." t="0."/>\r
+<eng-data cg="149." f="341.398" m="299.677" t="0.02"/>\r
+<eng-data cg="149." f="365.497" m="280.441" t="0.1"/>\r
+<eng-data cg="149." f="383.571" m="254.96" t="0.2"/>\r
+<eng-data cg="149." f="403.653" m="228.181" t="0.3"/>\r
+<eng-data cg="149." f="405.662" m="200.651" t="0.4"/>\r
+<eng-data cg="149." f="405.662" m="173.053" t="0.5"/>\r
+<eng-data cg="149." f="404.657" m="145.489" t="0.6"/>\r
+<eng-data cg="149." f="374.534" m="118.984" t="0.7"/>\r
+<eng-data cg="149." f="342.402" m="94.596" t="0.8"/>\r
+<eng-data cg="149." f="309.267" m="72.4285" t="0.9"/>\r
+<eng-data cg="149." f="272.115" m="52.652" t="1."/>\r
+<eng-data cg="149." f="238.979" m="35.2664" t="1.1"/>\r
+<eng-data cg="149." f="224.921" m="27.3763" t="1.15"/>\r
+<eng-data cg="149." f="194.798" m="20.2376" t="1.2"/>\r
+<eng-data cg="149." f="119.489" m="9.54671" t="1.3"/>\r
+<eng-data cg="149." f="62.255" m="3.36443" t="1.4"/>\r
+<eng-data cg="149." f="33.136" m="1.742" t="1.45"/>\r
+<eng-data cg="149." f="23.095" m="0.785609" t="1.5"/>\r
+<eng-data cg="149." f="0." m="0." t="1.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech I357T\r
-; Copyright Tripoli Motor Testing 1997 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I357T 38 203 14 0.1792 0.34944 AT\r
- 0.028 311.629\r
- 0.087 351.768\r
- 0.147 349.074\r
- 0.206 346.175\r
- 0.266 341.229\r
- 0.325 336.857\r
- 0.384 333.748\r
- 0.444 326.960\r
- 0.503 319.679\r
- 0.563 312.533\r
- 0.622 300.790\r
- 0.681 292.787\r
- 0.741 283.766\r
- 0.800 274.578\r
- 0.859 264.915\r
- 0.919 254.273\r
- 0.978 241.755\r
- 1.037 229.020\r
- 1.097 216.238\r
- 1.156 187.776\r
- 1.216 109.940\r
- 1.275 56.459\r
- 1.334 24.476\r
- 1.394 10.977\r
- 1.454 3.450\r
- 1.515 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="209.22" Itot="341." Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="310." burn-time="1.1" cgDiv="10" cgFix="1" cgStep="-1." code="I357T" delays="6,10,14" dia="38." exitDia="0." initWt="363.5" len="202." mDiv="10" mFix="1" mStep="-1." massFrac="45.72" mfg="Aerotech" peakThrust="465.53" propWt="166.2" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="101." f="0." m="166.2" t="0."/>\r
+<eng-data cg="101." f="465.53" m="166.2" t="0."/>\r
+<eng-data cg="101." f="407.97" m="144.913" t="0.1"/>\r
+<eng-data cg="101." f="394.67" m="86.2334" t="0.4"/>\r
+<eng-data cg="101." f="363.62" m="49.2751" t="0.6"/>\r
+<eng-data cg="101." f="319.23" m="32.6344" t="0.7"/>\r
+<eng-data cg="101." f="257.18" m="18.5876" t="0.8"/>\r
+<eng-data cg="101." f="190.69" m="7.67322" t="0.9"/>\r
+<eng-data cg="101." f="62.09" m="1.5131" t="1."/>\r
+<eng-data cg="101." f="0." m="0." t="1.1"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech I364FJ\r
-; Curvefit to instruction sheet on Aerotech website (12/27/06)\r
-; by Chris Kobel\r
-; burn time: 1.7 seconds\r
-; total impulse: 551.2 newton-seconds\r
-; average thrust: 72.9 pounds\r
-I364FJ 38 345 6-10-14 0.3625 0.678 AT\r
- 0.02 356.0\r
- 0.10 373.8\r
- 0.20 387.2\r
- 0.30 400.5\r
- 0.40 400.5\r
- 0.50 409.4\r
- 0.60 413.9\r
- 0.70 409.4\r
- 0.80 382.7\r
- 0.90 373.8\r
- 1.00 351.6\r
- 1.10 333.8\r
- 1.20 320.4\r
- 1.30 311.5\r
- 1.40 244.8\r
- 1.50 178.0\r
- 1.60 80.1\r
- 1.70 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="155.05" Itot="551.202" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="324.236" burn-time="1.7" cgDiv="10" cgFix="1" cgStep="-1." code="I364FJ" delays="6,10,14" dia="38." exitDia="0." initWt="678." len="345." mDiv="10" mFix="1" mStep="-1." massFrac="53.47" mfg="Aerotech" peakThrust="413.9" propWt="362.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AeroTech I364FJ\r
+Curvefit to instruction sheet on Aerotech website (12/27/06)\r
+by Chris Kobel\r
+burn time: 1.7 seconds\r
+total impulse: 551.2 newton-seconds\r
+average thrust: 72.9 pounds\r
+</comments>\r
+<data>\r
+<eng-data cg="172.5" f="0." m="362.5" t="0."/>\r
+<eng-data cg="172.5" f="356." m="360.159" t="0.02"/>\r
+<eng-data cg="172.5" f="373.8" m="340.961" t="0.1"/>\r
+<eng-data cg="172.5" f="387.2" m="315.937" t="0.2"/>\r
+<eng-data cg="172.5" f="400.5" m="290.035" t="0.3"/>\r
+<eng-data cg="172.5" f="400.5" m="263.696" t="0.4"/>\r
+<eng-data cg="172.5" f="409.4" m="237.064" t="0.5"/>\r
+<eng-data cg="172.5" f="413.9" m="209.992" t="0.6"/>\r
+<eng-data cg="172.5" f="409.4" m="182.92" t="0.7"/>\r
+<eng-data cg="172.5" f="382.7" m="156.873" t="0.8"/>\r
+<eng-data cg="172.5" f="373.8" m="131.998" t="0.9"/>\r
+<eng-data cg="172.5" f="351.6" m="108.145" t="1."/>\r
+<eng-data cg="172.5" f="333.8" m="85.6068" t="1.1"/>\r
+<eng-data cg="172.5" f="320.4" m="64.0949" t="1.2"/>\r
+<eng-data cg="172.5" f="311.5" m="43.3164" t="1.3"/>\r
+<eng-data cg="172.5" f="244.8" m="25.0237" t="1.4"/>\r
+<eng-data cg="172.5" f="178." m="11.1209" t="1.5"/>\r
+<eng-data cg="172.5" f="80.1" m="2.6339" t="1.6"/>\r
+<eng-data cg="172.5" f="0." m="0." t="1.7"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech I366R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I366R 38 298 0 0.3136 0.55552 AT\r
- 0.027 323.256\r
- 0.088 485.393\r
- 0.148 483.744\r
- 0.208 479.926\r
- 0.268 473.365\r
- 0.327 466.192\r
- 0.388 457.444\r
- 0.448 448.751\r
- 0.509 441.477\r
- 0.570 430.236\r
- 0.630 421.524\r
- 0.690 411.757\r
- 0.750 398.876\r
- 0.810 387.496\r
- 0.870 375.430\r
- 0.930 361.325\r
- 0.991 345.057\r
- 1.053 330.392\r
- 1.112 312.636\r
- 1.173 293.508\r
- 1.233 275.085\r
- 1.292 262.408\r
- 1.353 230.881\r
- 1.413 118.008\r
- 1.474 23.611\r
- 1.535 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="172.22" Itot="537.064" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="358.043" burn-time="1.5" cgDiv="10" cgFix="1" cgStep="-1." code="I366R" delays="10,14" dia="38." exitDia="0." initWt="562." len="298." mDiv="10" mFix="1" mStep="-1." massFrac="56.58" mfg="Aerotech" peakThrust="485.39" propWt="318." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="149." f="0." m="318." t="0."/>\r
+<eng-data cg="149." f="323.26" m="315.129" t="0.03"/>\r
+<eng-data cg="149." f="485.39" m="300.765" t="0.09"/>\r
+<eng-data cg="149." f="483.74" m="283.55" t="0.15"/>\r
+<eng-data cg="149." f="479.93" m="266.432" t="0.21"/>\r
+<eng-data cg="149." f="473.37" m="249.498" t="0.27"/>\r
+<eng-data cg="149." f="466.19" m="232.809" t="0.33"/>\r
+<eng-data cg="149." f="457.44" m="216.402" t="0.39"/>\r
+<eng-data cg="149." f="448.75" m="200.305" t="0.45"/>\r
+<eng-data cg="149." f="441.48" m="184.492" t="0.51"/>\r
+<eng-data cg="149." f="430.24" m="169.007" t="0.57"/>\r
+<eng-data cg="149." f="421.52" m="153.877" t="0.63"/>\r
+<eng-data cg="149." f="411.76" m="139.075" t="0.69"/>\r
+<eng-data cg="149." f="398.88" m="124.676" t="0.75"/>\r
+<eng-data cg="149." f="387.5" m="110.707" t="0.81"/>\r
+<eng-data cg="149." f="375.43" m="97.155" t="0.87"/>\r
+<eng-data cg="149." f="361.32" m="84.068" t="0.93"/>\r
+<eng-data cg="149." f="345.06" m="71.5204" t="0.99"/>\r
+<eng-data cg="149." f="330.39" m="59.5222" t="1.05"/>\r
+<eng-data cg="149." f="312.64" m="48.0999" t="1.11"/>\r
+<eng-data cg="149." f="293.51" m="37.3327" t="1.17"/>\r
+<eng-data cg="149." f="275.08" m="27.2327" t="1.23"/>\r
+<eng-data cg="149." f="262.41" m="17.6852" t="1.29"/>\r
+<eng-data cg="149." f="230.88" m="8.92274" t="1.35"/>\r
+<eng-data cg="149." f="118.01" m="2.72532" t="1.41"/>\r
+<eng-data cg="149." f="23.61" m="0.209695" t="1.47"/>\r
+<eng-data cg="149." f="0." m="0." t="1.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech I435T\r
-; Copyright Tripoli Motor Testing 1996 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I435T 38 298 6 0.28672 0.52864 AT\r
- 0.026 684.626\r
- 0.080 702.334\r
- 0.134 655.130\r
- 0.190 638.942\r
- 0.245 624.098\r
- 0.299 611.802\r
- 0.354 602.601\r
- 0.409 590.237\r
- 0.464 575.712\r
- 0.519 563.654\r
- 0.574 548.912\r
- 0.628 527.885\r
- 0.683 504.211\r
- 0.739 480.412\r
- 0.793 459.219\r
- 0.848 436.771\r
- 0.903 414.493\r
- 0.957 392.151\r
- 1.012 366.634\r
- 1.068 299.670\r
- 1.122 182.639\r
- 1.177 106.457\r
- 1.232 55.447\r
- 1.286 23.628\r
- 1.342 11.052\r
- 1.397 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="204.83" Itot="556.41" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="397.436" burn-time="1.4" cgDiv="10" cgFix="1" cgStep="-1." code="I435T" delays="6,10,14" dia="38." exitDia="0." initWt="526.9" len="297." mDiv="10" mFix="1" mStep="-1." massFrac="52.57" mfg="Aerotech" peakThrust="780.77" propWt="277." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="148.5" f="0." m="277." t="0."/>\r
+<eng-data cg="148.5" f="780.77" m="277." t="0."/>\r
+<eng-data cg="148.5" f="628.21" m="241.928" t="0.1"/>\r
+<eng-data cg="148.5" f="583.33" m="211.771" t="0.2"/>\r
+<eng-data cg="148.5" f="551.92" m="183.513" t="0.3"/>\r
+<eng-data cg="148.5" f="538.46" m="156.371" t="0.4"/>\r
+<eng-data cg="148.5" f="529.49" m="129.788" t="0.5"/>\r
+<eng-data cg="148.5" f="507.05" m="103.987" t="0.6"/>\r
+<eng-data cg="148.5" f="448.72" m="80.1961" t="0.7"/>\r
+<eng-data cg="148.5" f="403.85" m="58.9741" t="0.8"/>\r
+<eng-data cg="148.5" f="358.97" m="39.9863" t="0.9"/>\r
+<eng-data cg="148.5" f="314.1" m="23.2324" t="1."/>\r
+<eng-data cg="148.5" f="197.44" m="10.4993" t="1.1"/>\r
+<eng-data cg="148.5" f="89.74" m="3.35092" t="1.2"/>\r
+<eng-data cg="148.5" f="22.44" m="0.55857" t="1.3"/>\r
+<eng-data cg="148.5" f="0." m="0." t="1.4"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech I435T\r
-; Copyright Tripoli Motor Testing 1999 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I435T 38 297 0 0.26656 0.513408 AT\r
- 0.024 808.049\r
- 0.074 749.691\r
- 0.124 709.215\r
- 0.174 656.216\r
- 0.224 636.578\r
- 0.274 621.839\r
- 0.324 592.267\r
- 0.374 584.551\r
- 0.424 573.277\r
- 0.474 547.725\r
- 0.524 539.962\r
- 0.574 525.268\r
- 0.624 500.456\r
- 0.674 484.978\r
- 0.724 464.323\r
- 0.774 442.837\r
- 0.824 424.540\r
- 0.874 405.872\r
- 0.924 393.443\r
- 0.974 317.157\r
- 1.024 217.630\r
- 1.074 126.188\r
- 1.124 74.391\r
- 1.174 30.034\r
- 1.224 9.380\r
- 1.274 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Aerotech" code="I49N-P" Type="reloadable" dia="38." len="184."\r
+initWt="398." propWt="205." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="48.372" peakThrust="63.438" throatDia="0." exitDia="0." Itot="384.119"\r
+burn-time="7.94" massFrac="51.51" Isp="191.07" tDiv="10" tStep="-1." tFix="1"\r
+FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+ <comments>Aerotech I49N-P</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="205." cg="92."/>\r
+ <eng-data t="0.008" f="1.406" m="204.997" cg="92."/>\r
+ <eng-data t="0.025" f="48.594" m="204.77" cg="92."/>\r
+ <eng-data t="0.093" f="52.031" m="202.944" cg="92."/>\r
+ <eng-data t="0.429" f="57.344" m="193.138" cg="92."/>\r
+ <eng-data t="0.665" f="60.313" m="185.728" cg="92."/>\r
+ <eng-data t="0.841" f="60.625" m="180.048" cg="92."/>\r
+ <eng-data t="1.06" f="62.344" m="172.862" cg="92."/>\r
+ <eng-data t="1.295" f="63.438" m="164.975" cg="92."/>\r
+ <eng-data t="1.556" f="62.344" m="156.214" cg="92."/>\r
+ <eng-data t="1.825" f="62.344" m="147.264" cg="92."/>\r
+ <eng-data t="1.994" f="60.625" m="141.719" cg="92."/>\r
+ <eng-data t="2.212" f="60.156" m="134.693" cg="92."/>\r
+ <eng-data t="3.003" f="56.719" m="110.023" cg="92."/>\r
+ <eng-data t="3.785" f="52.344" m="87.2648" cg="92."/>\r
+ <eng-data t="4.349" f="49.375" m="71.9561" cg="92."/>\r
+ <eng-data t="4.997" f="46.563" m="55.367" cg="92."/>\r
+ <eng-data t="5.998" f="43.438" m="31.3267" cg="92."/>\r
+ <eng-data t="6.393" f="42.031" m="22.3179" cg="92."/>\r
+ <eng-data t="6.831" f="41.563" m="12.5476" cg="92."/>\r
+ <eng-data t="6.999" f="36.875" m="9.03125" cg="92."/>\r
+ <eng-data t="7.083" f="33.125" m="7.46221" cg="92."/>\r
+ <eng-data t="7.184" f="31.406" m="5.72301" cg="92."/>\r
+ <eng-data t="7.369" f="23.125" m="3.03102" cg="92."/>\r
+ <eng-data t="7.495" f="16.406" m="1.70189" cg="92."/>\r
+ <eng-data t="7.764" f="4.219" m="0.221405" cg="92."/>\r
+ <eng-data t="7.882" f="1.875" m="0.0295197" cg="92."/>\r
+ <eng-data t="7.941" f="0." m="0." cg="92."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Aerotech" code="I59WN-P" Type="reloadable" dia="38." len="232."\r
+initWt="487." propWt="272." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="56.567" peakThrust="171.786" throatDia="0." exitDia="0."\r
+Itot="486.706" burn-time="8.6" massFrac="55.85" Isp="182.46" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Aerotech I59WN-P</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="272." cg="116."/>\r
+ <eng-data t="0.009" f="0.357" m="271.999" cg="116."/>\r
+ <eng-data t="0.046" f="138.571" m="270.563" cg="116."/>\r
+ <eng-data t="0.12" f="150." m="264.596" cg="116."/>\r
+ <eng-data t="0.193" f="147.857" m="258.52" cg="116."/>\r
+ <eng-data t="0.368" f="157.857" m="243.57" cg="116."/>\r
+ <eng-data t="0.506" f="167.857" m="231.01" cg="116."/>\r
+ <eng-data t="0.699" f="171.071" m="212.732" cg="116."/>\r
+ <eng-data t="0.791" f="171.786" m="203.918" cg="116."/>\r
+ <eng-data t="0.893" f="168.571" m="194.217" cg="116."/>\r
+ <eng-data t="1.058" f="158.214" m="179.151" cg="116."/>\r
+ <eng-data t="1.233" f="146.429" m="164.253" cg="116."/>\r
+ <eng-data t="1.417" f="132.143" m="149.931" cg="116."/>\r
+ <eng-data t="1.509" f="125.714" m="143.302" cg="116."/>\r
+ <eng-data t="1.61" f="100.357" m="136.922" cg="116."/>\r
+ <eng-data t="1.675" f="80.357" m="133.639" cg="116."/>\r
+ <eng-data t="1.785" f="60.357" m="129.314" cg="116."/>\r
+ <eng-data t="1.96" f="53.571" m="123.743" cg="116."/>\r
+ <eng-data t="2.209" f="48.571" m="116.636" cg="116."/>\r
+ <eng-data t="2.531" f="45.357" m="108.185" cg="116."/>\r
+ <eng-data t="2.669" f="43.214" m="104.769" cg="116."/>\r
+ <eng-data t="3.009" f="40.714" m="96.7958" cg="116."/>\r
+ <eng-data t="3.387" f="40.714" m="88.195" cg="116."/>\r
+ <eng-data t="4.021" f="38.929" m="74.0856" cg="116."/>\r
+ <eng-data t="4.261" f="37.5" m="68.96" cg="116."/>\r
+ <eng-data t="4.997" f="36.429" m="53.7557" cg="116."/>\r
+ <eng-data t="6." f="33.929" m="34.0366" cg="116."/>\r
+ <eng-data t="6.883" f="31.429" m="17.9104" cg="116."/>\r
+ <eng-data t="7.003" f="33.571" m="15.7309" cg="116."/>\r
+ <eng-data t="7.187" f="30.714" m="12.4257" cg="116."/>\r
+ <eng-data t="7.334" f="27.5" m="10.0345" cg="116."/>\r
+ <eng-data t="7.574" f="22.5" m="6.6813" cg="116."/>\r
+ <eng-data t="7.96" f="17.5" m="2.3669" cg="116."/>\r
+ <eng-data t="8.117" f="9.643" m="1.17613" cg="116."/>\r
+ <eng-data t="8.319" f="4.643" m="0.369757" cg="116."/>\r
+ <eng-data t="8.604" f="0." m="0." cg="116."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;I600R Data Entered by Tim Van Milligan\r
-;For RockSim: www.RockSim.com\r
-;Based on Aerotech's Reload Kit Instruction Sheet.\r
-;Not Officially Approved by TRA or Aerotech\r
-I600R 38 344.68 6-10-14 0.3237 0.617 AT\r
-0.005 40.438\r
-0.046 817.754\r
-0.059 813.261\r
-0.1 772.822\r
-0.2 736.877\r
-0.4 696.439\r
-0.5 669.48\r
-0.6 620.055\r
-0.796 539.178\r
-0.894 485.261\r
-0.951 453.809\r
-0.964 435.836\r
-1 274.082\r
-1.052 152.767\r
-1.106 62.904\r
-1.144 13.48\r
-1.18 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="201.66" Itot="640.142" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="542.493" burn-time="1.18" cgDiv="10" cgFix="1" cgStep="-1." code="I600R" delays="10" dia="38." exitDia="0." initWt="617." len="344.68" mDiv="10" mFix="1" mStep="-1." massFrac="52.46" mfg="Aerotech" peakThrust="817.754" propWt="323.7" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>I600R Data Entered by Tim Van Milligan\r
+For RockSim: www.RockSim.com\r
+Based on Aerotech's Reload Kit Instruction Sheet.\r
+Not Officially Approved by TRA or Aerotech\r
+</comments>\r
+<data>\r
+<eng-data cg="172.34" f="0." m="323.7" t="0."/>\r
+<eng-data cg="172.34" f="40.438" m="323.649" t="0.005"/>\r
+<eng-data cg="172.34" f="817.754" m="314.753" t="0.046"/>\r
+<eng-data cg="172.34" f="813.261" m="309.392" t="0.059"/>\r
+<eng-data cg="172.34" f="772.822" m="292.95" t="0.1"/>\r
+<eng-data cg="172.34" f="736.877" m="254.78" t="0.2"/>\r
+<eng-data cg="172.34" f="696.439" m="182.301" t="0.4"/>\r
+<eng-data cg="172.34" f="669.48" m="147.766" t="0.5"/>\r
+<eng-data cg="172.34" f="620.055" m="115.162" t="0.6"/>\r
+<eng-data cg="172.34" f="539.178" m="57.7157" t="0.796"/>\r
+<eng-data cg="172.34" f="485.261" m="32.3324" t="0.894"/>\r
+<eng-data cg="172.34" f="453.809" m="18.7989" t="0.951"/>\r
+<eng-data cg="172.34" f="435.836" m="15.8748" t="0.964"/>\r
+<eng-data cg="172.34" f="274.082" m="9.4131" t="1."/>\r
+<eng-data cg="172.34" f="152.767" m="3.80114" t="1.052"/>\r
+<eng-data cg="172.34" f="62.904" m="0.856571" t="1.106"/>\r
+<eng-data cg="172.34" f="13.48" m="0.122696" t="1.144"/>\r
+<eng-data cg="172.34" f="0." m="0." t="1.18"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech I65W\r
-; Copyright Tripoli Motor Testing 1997 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I65W 54 235 0 0.41216 0.7616 AT\r
- 0.180 125.414\r
- 0.544 139.304\r
- 0.908 145.369\r
- 1.273 148.283\r
- 1.638 146.745\r
- 2.002 139.049\r
- 2.367 131.200\r
- 2.731 123.276\r
- 3.096 113.454\r
- 3.460 102.368\r
- 3.825 90.210\r
- 4.190 78.084\r
- 4.554 66.812\r
- 4.919 55.780\r
- 5.283 47.281\r
- 5.648 39.154\r
- 6.012 32.528\r
- 6.377 27.069\r
- 6.742 22.099\r
- 7.106 18.095\r
- 7.471 14.819\r
- 7.835 12.097\r
- 8.200 9.763\r
- 8.565 7.875\r
- 8.929 5.999\r
- 9.294 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="173.91" Itot="630.5" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="76.332" burn-time="8.26" cgDiv="10" cgFix="1" cgStep="-1." code="I65W" delays="1000" dia="54." exitDia="0." initWt="776.1" len="235." mDiv="10" mFix="1" mStep="-1." massFrac="47.64" mfg="Aerotech" peakThrust="150.07" propWt="369.7" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AEROTECH I65 RASP.ENG file made from NAR published data\r
+File produced OCT 3, 2002\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="117.5" f="0." m="369.7" t="0."/>\r
+<eng-data cg="117.5" f="55.739" m="368.295" t="0.086"/>\r
+<eng-data cg="117.5" f="90.267" m="367.738" t="0.099"/>\r
+<eng-data cg="117.5" f="113.911" m="364.805" t="0.148"/>\r
+<eng-data cg="117.5" f="113.911" m="354.92" t="0.296"/>\r
+<eng-data cg="117.5" f="121.767" m="337.922" t="0.542"/>\r
+<eng-data cg="117.5" f="123.588" m="335.26" t="0.579"/>\r
+<eng-data cg="117.5" f="128.953" m="317.047" t="0.825"/>\r
+<eng-data cg="117.5" f="132.593" m="305.698" t="0.973"/>\r
+<eng-data cg="117.5" f="138.725" m="301.8" t="1.022"/>\r
+<eng-data cg="117.5" f="132.593" m="297.903" t="1.071"/>\r
+<eng-data cg="117.5" f="138.629" m="277.308" t="1.33"/>\r
+<eng-data cg="117.5" f="139.875" m="263.264" t="1.502"/>\r
+<eng-data cg="117.5" f="150.07" m="244.392" t="1.724"/>\r
+<eng-data cg="117.5" f="141.886" m="219.142" t="2.019"/>\r
+<eng-data cg="117.5" f="131.923" m="161.825" t="2.733"/>\r
+<eng-data cg="117.5" f="119.181" m="131.862" t="3.14"/>\r
+<eng-data cg="117.5" f="122.151" m="126.697" t="3.213"/>\r
+<eng-data cg="117.5" f="114.295" m="122.399" t="3.275"/>\r
+<eng-data cg="117.5" f="103.948" m="103.524" t="3.57"/>\r
+<eng-data cg="117.5" f="88.791" m="80.5253" t="3.977"/>\r
+<eng-data cg="117.5" f="93.036" m="76.5805" t="4.051"/>\r
+<eng-data cg="117.5" f="84.547" m="74.0294" t="4.1"/>\r
+<eng-data cg="117.5" f="74.229" m="58.5748" t="4.432"/>\r
+<eng-data cg="117.5" f="58.44" m="39.9048" t="4.912"/>\r
+<eng-data cg="117.5" f="34.758" m="17.6906" t="5.725"/>\r
+<eng-data cg="117.5" f="24.43" m="10.8536" t="6.119"/>\r
+<eng-data cg="117.5" f="13.489" m="5.38396" t="6.611"/>\r
+<eng-data cg="117.5" f="6.787" m="2.08475" t="7.166"/>\r
+<eng-data cg="117.5" f="3.729" m="0.75903" t="7.596"/>\r
+<eng-data cg="117.5" f="1.886" m="0.13018" t="7.978"/>\r
+<eng-data cg="117.5" f="0.665" m="0.0284648" t="8.114"/>\r
+<eng-data cg="117.5" f="0." m="0." t="8.26"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
; AeroTech J125\r
-; Copyright Tripoli Motor Testing 1997 (www.tripoli.org)\r
+; converted from TMT test stand data 1997 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
J125 54 368 0 0.63392 1.288 AT\r
0.174 223.931\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="202.87" Itot="1279.8" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="124.98" burn-time="10.24" cgDiv="10" cgFix="1" cgStep="-1." code="J125W" delays="100" dia="54." exitDia="0." initWt="1115." len="368." mDiv="10" mFix="1" mStep="-1." massFrac="57.7" mfg="Aerotech" peakThrust="214." propWt="643.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="184." f="0." m="643.3" t="0."/>\r
+<eng-data cg="184." f="214." m="589.516" t="1."/>\r
+<eng-data cg="184." f="200." m="381.416" t="3."/>\r
+<eng-data cg="184." f="142." m="294.602" t="4.01"/>\r
+<eng-data cg="184." f="120." m="97.7165" t="7."/>\r
+<eng-data cg="184." f="0." m="0." t="10.24"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; AT 54-852\r
-; Greg Gardner - 09/15/06\r
-J1299N 54 230 0 0.3716 0.834 AT\r
-0.01 548\r
-0.02 1152\r
-0.03 1232\r
-0.04 1277\r
-0.05 1272\r
-0.06 1288\r
-0.07 1333\r
-0.08 1347\r
-0.09 1378\r
-0.10 1383\r
-0.12 1405\r
-0.14 1410\r
-0.16 1440\r
-0.18 1444\r
-0.20 1446\r
-0.25 1449\r
-0.30 1452\r
-0.35 1448\r
-0.40 1440\r
-0.45 1405\r
-0.50 1320\r
-0.55 1248\r
-0.57 1224\r
-0.59 1210\r
-0.60 1180\r
-0.61 1188\r
-0.615 1195\r
-0.62 1188\r
-0.63 510\r
-0.64 220\r
-0.65 96\r
-0.66 46\r
-0.67 26\r
-0.678 0\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="233.3" Itot="850.164" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1253.93" burn-time="0.68" cgDiv="10" cgFix="1" cgStep="-1." code="J1299N" delays="1000" dia="54." exitDia="0." initWt="834." len="230." mDiv="10" mFix="1" mStep="-1." massFrac="44.56" mfg="Aerotech" peakThrust="1452." propWt="371.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AT 54-852\r
+Greg Gardner - 09/15/06\r
+</comments>\r
+<data>\r
+<eng-data cg="115." f="0." m="371.6" t="0."/>\r
+<eng-data cg="115." f="548." m="370.402" t="0.01"/>\r
+<eng-data cg="115." f="1152." m="366.687" t="0.02"/>\r
+<eng-data cg="115." f="1232." m="361.477" t="0.03"/>\r
+<eng-data cg="115." f="1277." m="355.994" t="0.04"/>\r
+<eng-data cg="115." f="1272." m="350.423" t="0.05"/>\r
+<eng-data cg="115." f="1288." m="344.828" t="0.06"/>\r
+<eng-data cg="115." f="1333." m="339.1" t="0.07"/>\r
+<eng-data cg="115." f="1347." m="333.243" t="0.08"/>\r
+<eng-data cg="115." f="1378." m="327.288" t="0.09"/>\r
+<eng-data cg="115." f="1383." m="321.254" t="0.1"/>\r
+<eng-data cg="115." f="1405." m="309.067" t="0.12"/>\r
+<eng-data cg="115." f="1410." m="296.763" t="0.14"/>\r
+<eng-data cg="115." f="1440." m="284.306" t="0.16"/>\r
+<eng-data cg="115." f="1444." m="271.7" t="0.18"/>\r
+<eng-data cg="115." f="1446." m="259.068" t="0.2"/>\r
+<eng-data cg="115." f="1449." m="227.434" t="0.25"/>\r
+<eng-data cg="115." f="1452." m="195.734" t="0.3"/>\r
+<eng-data cg="115." f="1448." m="164.045" t="0.35"/>\r
+<eng-data cg="115." f="1440." m="132.487" t="0.4"/>\r
+<eng-data cg="115." f="1405." m="101.398" t="0.45"/>\r
+<eng-data cg="115." f="1320." m="71.6215" t="0.5"/>\r
+<eng-data cg="115." f="1248." m="43.5602" t="0.55"/>\r
+<eng-data cg="115." f="1224." m="32.7552" t="0.57"/>\r
+<eng-data cg="115." f="1210." m="22.1164" t="0.59"/>\r
+<eng-data cg="115." f="1180." m="16.8932" t="0.6"/>\r
+<eng-data cg="115." f="1188." m="11.718" t="0.61"/>\r
+<eng-data cg="115." f="1195." m="14.322" t="0.605"/>\r
+<eng-data cg="115." f="1188." m="6.51005" t="0.62"/>\r
+<eng-data cg="115." f="510." m="2.79914" t="0.63"/>\r
+<eng-data cg="115." f="220." m="1.20375" t="0.64"/>\r
+<eng-data cg="115." f="96." m="0.513146" t="0.65"/>\r
+<eng-data cg="115." f="46." m="0.202811" t="0.66"/>\r
+<eng-data cg="115." f="26." m="0.0454576" t="0.67"/>\r
+<eng-data cg="115." f="0." m="0." t="0.678"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech J135W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J135W 54 368 0 0.62272 1.14106 AT\r
- 0.147 226.295\r
- 0.444 243.688\r
- 0.742 250.916\r
- 1.040 257.345\r
- 1.338 259.308\r
- 1.635 253.727\r
- 1.933 246.071\r
- 2.231 235.780\r
- 2.529 221.775\r
- 2.827 205.143\r
- 3.125 183.570\r
- 3.423 161.103\r
- 3.720 140.983\r
- 4.017 122.984\r
- 4.315 106.605\r
- 4.612 91.959\r
- 4.910 77.693\r
- 5.208 65.304\r
- 5.506 54.347\r
- 5.804 44.246\r
- 6.102 35.395\r
- 6.400 27.716\r
- 6.698 21.121\r
- 6.996 14.939\r
- 7.294 9.737\r
- 7.592 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="191.63" Itot="1103.33" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="157.619" burn-time="7." cgDiv="10" cgFix="1" cgStep="-1." code="J135W" delays="6,10,14" dia="54." exitDia="0." initWt="1125.7" len="368." mDiv="10" mFix="1" mStep="-1." massFrac="52.15" mfg="Aerotech" peakThrust="270.44" propWt="587.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="184." f="0." m="587.1" t="0."/>\r
+<eng-data cg="184." f="152.12" m="587.1" t="0."/>\r
+<eng-data cg="184." f="239.75" m="430.71" t="1.5"/>\r
+<eng-data cg="184." f="260.21" m="364.2" t="2."/>\r
+<eng-data cg="184." f="270.44" m="293.609" t="2.5"/>\r
+<eng-data cg="184." f="265.55" m="222.306" t="3."/>\r
+<eng-data cg="184." f="233.52" m="155.915" t="3.5"/>\r
+<eng-data cg="184." f="176.14" m="101.419" t="4."/>\r
+<eng-data cg="184." f="127.66" m="61.0045" t="4.5"/>\r
+<eng-data cg="184." f="85.4" m="32.6613" t="5."/>\r
+<eng-data cg="184." f="48.48" m="14.8514" t="5.5"/>\r
+<eng-data cg="184." f="23.57" m="5.26662" t="6."/>\r
+<eng-data cg="184." f="8.01" m="1.06556" t="6.5"/>\r
+<eng-data cg="184." f="0." m="0." t="7."/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech J145H\r
-; Copyright Tripoli Motor Testing 1999 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J145H 54 709 0 0.410816 1.79738 AT\r
- 0.113 253.118\r
- 0.340 293.672\r
- 0.567 300.149\r
- 0.794 289.519\r
- 1.021 253.366\r
- 1.248 251.809\r
- 1.476 246.042\r
- 1.704 236.553\r
- 1.931 229.907\r
- 2.158 222.550\r
- 2.385 211.120\r
- 2.612 201.066\r
- 2.841 191.143\r
- 3.069 139.197\r
- 3.296 79.889\r
- 3.523 63.900\r
- 3.750 51.048\r
- 3.977 40.565\r
- 4.205 31.710\r
- 4.433 24.429\r
- 4.660 19.950\r
- 4.887 15.256\r
- 5.115 12.412\r
- 5.342 10.212\r
- 5.570 9.135\r
- 5.798 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="203.92" Itot="821.554" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="141.696" burn-time="5.8" cgDiv="10" cgFix="1" cgStep="-1." code="J145H" delays="1000" dia="54." exitDia="0." initWt="1797.38" len="709." mDiv="10" mFix="1" mStep="-1." massFrac="22.86" mfg="Aerotech" peakThrust="300.149" propWt="410.816" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AeroTech J145H\r
+Copyright Tripoli Motor Testing 1999 (www.tripoli.org)\r
+provided by ThrustCurve.org (www.thrustcurve.org)\r
+</comments>\r
+<data>\r
+<eng-data cg="354.5" f="0." m="410.816" t="0."/>\r
+<eng-data cg="354.5" f="253.118" m="403.665" t="0.113"/>\r
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+<eng-data cg="354.5" f="300.149" m="338.929" t="0.567"/>\r
+<eng-data cg="354.5" f="289.519" m="305.462" t="0.794"/>\r
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+<eng-data cg="354.5" f="251.809" m="245.979" t="1.248"/>\r
+<eng-data cg="354.5" f="246.042" m="217.599" t="1.476"/>\r
+<eng-data cg="354.5" f="236.553" m="190.088" t="1.704"/>\r
+<eng-data cg="354.5" f="229.907" m="163.614" t="1.931"/>\r
+<eng-data cg="354.5" f="222.55" m="137.935" t="2.158"/>\r
+<eng-data cg="354.5" f="211.12" m="113.322" t="2.385"/>\r
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+<eng-data cg="354.5" f="191.143" m="67.4718" t="2.841"/>\r
+<eng-data cg="354.5" f="139.197" m="48.6406" t="3.069"/>\r
+<eng-data cg="354.5" f="79.889" m="36.2063" t="3.296"/>\r
+<eng-data cg="354.5" f="63.9" m="28.0455" t="3.523"/>\r
+<eng-data cg="354.5" f="51.048" m="21.5216" t="3.75"/>\r
+<eng-data cg="354.5" f="40.565" m="16.3221" t="3.977"/>\r
+<eng-data cg="354.5" f="31.71" m="12.202" t="4.205"/>\r
+<eng-data cg="354.5" f="24.429" m="9.00177" t="4.433"/>\r
+<eng-data cg="354.5" f="19.95" m="6.48302" t="4.66"/>\r
+<eng-data cg="354.5" f="15.256" m="4.48489" t="4.887"/>\r
+<eng-data cg="354.5" f="12.412" m="2.90766" t="5.115"/>\r
+<eng-data cg="354.5" f="10.212" m="1.62363" t="5.342"/>\r
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+<eng-data cg="354.5" f="0." m="0." t="5.798"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech J180T\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J180T 54 230 0 0.429184 0.809088 AT\r
- 0.093 301.634\r
- 0.281 313.236\r
- 0.470 313.710\r
- 0.658 308.334\r
- 0.847 300.100\r
- 1.035 290.743\r
- 1.224 278.867\r
- 1.412 263.823\r
- 1.601 245.974\r
- 1.790 226.651\r
- 1.978 207.345\r
- 2.167 187.053\r
- 2.355 168.339\r
- 2.544 149.993\r
- 2.732 133.094\r
- 2.921 116.330\r
- 3.109 100.088\r
- 3.298 84.507\r
- 3.486 70.453\r
- 3.675 57.263\r
- 3.864 44.453\r
- 4.052 33.340\r
- 4.241 24.654\r
- 4.429 17.964\r
- 4.619 12.391\r
- 4.808 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="211.47" Itot="825.773" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="183.505" burn-time="4.5" cgDiv="10" cgFix="1" cgStep="-1." code="J180T" delays="6,10,14" dia="54." exitDia="0." initWt="840.9" len="230." mDiv="10" mFix="1" mStep="-1." massFrac="47.35" mfg="Aerotech" peakThrust="360.56" propWt="398.2" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="115." f="0." m="398.2" t="0."/>\r
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+<eng-data cg="115." f="0." m="0." t="4.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; AT 54-1280\r
-; Greg Gardner - 09/15/06\r
-J1999N 54 314 0 0.5574 1.111 AT\r
-0.01 830\r
-0.02 1716\r
-0.03 1787\r
-0.04 1873\r
-0.05 1896\r
-0.06 1918\r
-0.07 1984\r
-0.08 2007\r
-0.09 2051\r
-0.10 2058\r
-0.12 2090\r
-0.14 2098\r
-0.16 2135\r
-0.18 2138\r
-0.20 2142\r
-0.25 2146\r
-0.30 2150\r
-0.35 2146\r
-0.40 2138\r
-0.45 2096\r
-0.50 1974\r
-0.55 1864\r
-0.57 1829\r
-0.59 1815\r
-0.60 1762\r
-0.61 1673\r
-0.62 1085\r
-0.63 490\r
-0.64 190\r
-0.65 81\r
-0.66 31\r
-0.67 0\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="228.74" Itot="1250.35" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1866.19" burn-time="0.67" cgDiv="10" cgFix="1" cgStep="-1." code="J1999N" delays="1000" dia="54." exitDia="0." initWt="1111." len="314." mDiv="10" mFix="1" mStep="-1." massFrac="50.17" mfg="Aerotech" peakThrust="2150." propWt="557.4" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AT 54-852\r
+Greg Gardner - 09/15/06\r
+</comments>\r
+<data>\r
+<eng-data cg="157." f="0." m="557.4" t="0."/>\r
+<eng-data cg="157." f="830." m="555.55" t="0.01"/>\r
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+<eng-data cg="157." f="1085." m="5.94916" t="0.62"/>\r
+<eng-data cg="157." f="490." m="2.43851" t="0.63"/>\r
+<eng-data cg="157." f="190." m="0.9228" t="0.64"/>\r
+<eng-data cg="157." f="81." m="0.318745" t="0.65"/>\r
+<eng-data cg="157." f="31." m="0.0690985" t="0.66"/>\r
+<eng-data cg="157." f="0." m="0." t="0.67"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J210H 54 609.6 100 0.471 1.497 Aerotech\r
-0.00772798 651.819\r
-0.0695518 528.502\r
-0.200927 488.864\r
-0.502318 409.589\r
-0.996909 374.355\r
-1.4915 312.697\r
-1.59196 286.272\r
-2.00927 167.359\r
-2.43431 88.0836\r
-2.50386 101.296\r
-2.55023 74.8711\r
-3.02164 57.2543\r
-4 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="184.86" Itot="853.842" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="213.461" burn-time="4." cgDiv="10" cgFix="1" cgStep="-1." code="J210H" delays="1000" dia="54." exitDia="0." initWt="1497." len="609.6" mDiv="10" mFix="1" mStep="-1." massFrac="31.46" mfg="Aerotech" peakThrust="651.819" propWt="471." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="304.8" f="0." m="471." t="0."/>\r
+<eng-data cg="304.8" f="651.819" m="469.611" t="0.00772798"/>\r
+<eng-data cg="304.8" f="528.502" m="449.484" t="0.0695518"/>\r
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+<eng-data cg="304.8" f="409.589" m="337.934" t="0.502318"/>\r
+<eng-data cg="304.8" f="374.355" m="230.993" t="0.996909"/>\r
+<eng-data cg="304.8" f="312.697" m="137.269" t="1.4915"/>\r
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+<eng-data cg="304.8" f="167.359" m="68.4605" t="2.00927"/>\r
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+<eng-data cg="304.8" f="74.8711" m="32.6287" t="2.55023"/>\r
+<eng-data cg="304.8" f="57.2543" m="15.4497" t="3.02164"/>\r
+<eng-data cg="304.8" f="0." m="0." t="4."/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J260HW 54 708.66 100 0.558 1.574 AT\r
-0.00772798 598.969\r
-0.0386399 475.651\r
-0.108192 506.481\r
-0.463679 493.268\r
-0.780526 475.651\r
-1.01236 427.205\r
-2.00155 330.314\r
-2.48841 193.784\r
-2.99073 114.509\r
-4.01082 57.2543\r
-4.5 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="213.85" Itot="1170.22" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="260.049" burn-time="4.5" cgDiv="10" cgFix="1" cgStep="-1." code="J260HW" delays="1000" dia="54." exitDia="0." initWt="1574." len="708.66" mDiv="10" mFix="1" mStep="-1." massFrac="35.45" mfg="Aerotech" peakThrust="598.969" propWt="558." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="354.33" f="0." m="558." t="0."/>\r
+<eng-data cg="354.33" f="598.969" m="556.896" t="0.00772798"/>\r
+<eng-data cg="354.33" f="475.651" m="548.977" t="0.0386399"/>\r
+<eng-data cg="354.33" f="506.481" m="532.69" t="0.108192"/>\r
+<eng-data cg="354.33" f="493.268" m="447.958" t="0.463679"/>\r
+<eng-data cg="354.33" f="475.651" m="374.764" t="0.780526"/>\r
+<eng-data cg="354.33" f="427.205" m="324.861" t="1.01236"/>\r
+<eng-data cg="354.33" f="330.314" m="146.208" t="2.00155"/>\r
+<eng-data cg="354.33" f="193.784" m="85.373" t="2.48841"/>\r
+<eng-data cg="354.33" f="114.509" m="48.4514" t="2.99073"/>\r
+<eng-data cg="354.33" f="57.2543" m="6.67749" t="4.01082"/>\r
+<eng-data cg="354.33" f="0." m="0." t="4.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech J275W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J275W 54 230 0 0.468608 0.864192 AT\r
- 0.075 239.740\r
- 0.227 289.133\r
- 0.380 299.773\r
- 0.533 312.721\r
- 0.686 323.878\r
- 0.840 332.165\r
- 0.992 336.422\r
- 1.145 335.110\r
- 1.298 329.538\r
- 1.451 325.343\r
- 1.604 309.980\r
- 1.756 292.901\r
- 1.909 275.732\r
- 2.063 257.341\r
- 2.216 234.891\r
- 2.369 213.102\r
- 2.521 182.501\r
- 2.674 167.853\r
- 2.827 153.041\r
- 2.980 138.115\r
- 3.133 105.605\r
- 3.285 67.369\r
- 3.439 29.239\r
- 3.592 14.599\r
- 3.745 6.662\r
- 3.898 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="189.65" Itot="818.693" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="255.842" burn-time="3.2" cgDiv="10" cgFix="1" cgStep="-1." code="J275W" delays="6,10,14,18" dia="54." exitDia="0." initWt="882.9" len="241." mDiv="10" mFix="1" mStep="-1." massFrac="49.86" mfg="Aerotech" peakThrust="350.5" propWt="440.2" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="120.5" f="0." m="440.2" t="0."/>\r
+<eng-data cg="120.5" f="0.45" m="440.2" t="0."/>\r
+<eng-data cg="120.5" f="331.55" m="431.274" t="0.1"/>\r
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+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech J315R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J315R 54 243 0 0.42112 0.8512 AT\r
- 0.051 189.719\r
- 0.154 337.529\r
- 0.259 354.534\r
- 0.363 364.111\r
- 0.468 371.479\r
- 0.572 373.222\r
- 0.676 376.062\r
- 0.780 372.962\r
- 0.884 368.988\r
- 0.989 366.978\r
- 1.093 358.752\r
- 1.197 351.302\r
- 1.301 339.336\r
- 1.406 325.202\r
- 1.510 311.322\r
- 1.614 300.496\r
- 1.718 288.598\r
- 1.822 278.279\r
- 1.927 270.538\r
- 2.031 262.127\r
- 2.136 245.027\r
- 2.239 236.238\r
- 2.344 188.308\r
- 2.448 63.668\r
- 2.552 18.746\r
- 2.657 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="179.95" Itot="757.065" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="291.179" burn-time="2.6" cgDiv="10" cgFix="1" cgStep="-1." code="J315R" delays="14,1000" dia="54." exitDia="0." initWt="863." len="230." mDiv="10" mFix="1" mStep="-1." massFrac="49.71" mfg="Aerotech" peakThrust="376.06" propWt="429." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="115." f="0." m="429." t="0."/>\r
+<eng-data cg="115." f="189.72" m="426.312" t="0.05"/>\r
+<eng-data cg="115." f="337.53" m="411.374" t="0.15"/>\r
+<eng-data cg="115." f="354.53" m="389.805" t="0.26"/>\r
+<eng-data cg="115." f="364.11" m="369.443" t="0.36"/>\r
+<eng-data cg="115." f="371.48" m="346.518" t="0.47"/>\r
+<eng-data cg="115." f="373.22" m="325.418" t="0.57"/>\r
+<eng-data cg="115." f="376.06" m="302.066" t="0.68"/>\r
+<eng-data cg="115." f="372.96" m="280.844" t="0.78"/>\r
+<eng-data cg="115." f="368.99" m="259.822" t="0.88"/>\r
+<eng-data cg="115." f="366.98" m="236.884" t="0.99"/>\r
+<eng-data cg="115." f="358.75" m="216.322" t="1.09"/>\r
+<eng-data cg="115." f="351.3" m="194.192" t="1.2"/>\r
+<eng-data cg="115." f="339.34" m="174.624" t="1.3"/>\r
+<eng-data cg="115." f="325.2" m="153.913" t="1.41"/>\r
+<eng-data cg="115." f="311.32" m="135.879" t="1.51"/>\r
+<eng-data cg="115." f="300.5" m="118.544" t="1.61"/>\r
+<eng-data cg="115." f="288.6" m="100.184" t="1.72"/>\r
+<eng-data cg="115." f="278.28" m="84.1221" t="1.82"/>\r
+<eng-data cg="115." f="270.54" m="67.0174" t="1.93"/>\r
+<eng-data cg="115." f="262.13" m="51.9252" t="2.03"/>\r
+<eng-data cg="115." f="245.03" m="36.1188" t="2.14"/>\r
+<eng-data cg="115." f="236.24" m="22.483" t="2.24"/>\r
+<eng-data cg="115." f="188.31" m="10.4541" t="2.34"/>\r
+<eng-data cg="115." f="63.67" m="2.60084" t="2.45"/>\r
+<eng-data cg="115." f="18.75" m="0.265623" t="2.55"/>\r
+<eng-data cg="115." f="0." m="0." t="2.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-J350W-L 38 337 P 0.361 0.651 AT\r
- 0.041 841.443\r
- 0.051 767.077\r
- 0.088 698.219\r
- 0.173 644.51\r
- 0.256 621.098\r
- 0.298 564.635\r
- 0.547 543.977\r
- 0.783 487.514\r
- 0.989 418.656\r
- 1.16 359.438\r
- 1.192 340.158\r
- 1.213 320.878\r
- 1.287 216.214\r
- 1.319 179.031\r
- 1.342 126.699\r
- 1.386 84.007\r
- 1.427 53.709\r
- 1.48 45.446\r
- 1.591 20.657\r
- 1.695 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="190.43" Itot="700.304" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="368.581" burn-time="1.9" cgDiv="10" cgFix="1" cgStep="-1." code="J350W" delays="6,10,14" dia="38." exitDia="0." initWt="665." len="340." mDiv="10" mFix="1" mStep="-1." massFrac="56.39" mfg="Aerotech" peakThrust="705.97" propWt="375." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="170." f="0." m="375." t="0."/>\r
+<eng-data cg="170." f="705.97" m="375." t="0."/>\r
+<eng-data cg="170." f="598.37" m="340.077" t="0.1"/>\r
+<eng-data cg="170." f="571.28" m="308.761" t="0.2"/>\r
+<eng-data cg="170." f="562.33" m="278.41" t="0.3"/>\r
+<eng-data cg="170." f="545.92" m="248.737" t="0.4"/>\r
+<eng-data cg="170." f="517.35" m="220.269" t="0.5"/>\r
+<eng-data cg="170." f="506.91" m="192.846" t="0.6"/>\r
+<eng-data cg="170." f="460.65" m="166.94" t="0.7"/>\r
+<eng-data cg="170." f="448.72" m="142.592" t="0.8"/>\r
+<eng-data cg="170." f="400.75" m="97.1049" t="1."/>\r
+<eng-data cg="170." f="345.32" m="57.1541" t="1.2"/>\r
+<eng-data cg="170." f="269.23" m="24.2461" t="1.4"/>\r
+<eng-data cg="170." f="155.39" m="12.8773" t="1.5"/>\r
+<eng-data cg="170." f="44.76" m="2.1596" t="1.7"/>\r
+<eng-data cg="170." f="17.95" m="0.480595" t="1.8"/>\r
+<eng-data cg="170." f="0." m="0." t="1.9"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech J350W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J350W 38 337 0 0.375872 0.650944 AT\r
- 0.038 706.781\r
- 0.115 669.055\r
- 0.192 602.539\r
- 0.270 565.084\r
- 0.348 539.143\r
- 0.425 514.910\r
- 0.503 483.098\r
- 0.581 449.128\r
- 0.658 437.256\r
- 0.736 424.199\r
- 0.815 414.461\r
- 0.892 402.956\r
- 0.970 393.604\r
- 1.048 377.837\r
- 1.125 359.785\r
- 1.203 341.916\r
- 1.281 324.721\r
- 1.358 305.935\r
- 1.436 264.279\r
- 1.515 175.471\r
- 1.592 110.912\r
- 1.670 77.100\r
- 1.748 55.472\r
- 1.825 39.990\r
- 1.903 26.276\r
- 1.981 0.000\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="176.63" Itot="649.559" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="433.039" burn-time="1.5" cgDiv="10" cgFix="1" cgStep="-1." code="J350W-L" delays="14" dia="38." exitDia="0." initWt="665." len="337.01" mDiv="10" mFix="1" mStep="-1." massFrac="56.39" mfg="Aerotech" peakThrust="845.603" propWt="375." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="168.505" f="0." m="375." t="0."/>\r
+<eng-data cg="168.505" f="845.603" m="371.982" t="0.0123648"/>\r
+<eng-data cg="168.505" f="757.519" m="359.108" t="0.0401855"/>\r
+<eng-data cg="168.505" f="638.606" m="305.54" t="0.173107"/>\r
+<eng-data cg="168.505" f="572.543" m="286.088" t="0.228748"/>\r
+<eng-data cg="168.505" f="541.714" m="200.583" t="0.49459"/>\r
+<eng-data cg="168.505" f="488.864" m="138.051" t="0.704791"/>\r
+<eng-data cg="168.505" f="405.185" m="61.4653" t="1.00155"/>\r
+<eng-data cg="168.505" f="347.93" m="38.6174" t="1.10665"/>\r
+<eng-data cg="168.505" f="264.251" m="18.407" t="1.22102"/>\r
+<eng-data cg="168.505" f="70.4669" m="2.27939" t="1.38794"/>\r
+<eng-data cg="168.505" f="0." m="0." t="1.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J390HW-TURBO 54 708.66 100 0.69 1.74 AT\r
-0.015456 440.418\r
-0.100464 550.523\r
-0.193199 546.118\r
-0.301391 656.223\r
-0.502318 647.414\r
-0.973725 581.352\r
-1.48377 471.247\r
-1.98609 378.759\r
-2.17929 334.718\r
-2.30294 255.442\r
-2.49614 158.55\r
-3.01391 57.2543\r
-3.5 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="189.03" Itot="1279.11" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="365.461" burn-time="3.5" cgDiv="10" cgFix="1" cgStep="-1." code="J390HW-TURBO" delays="1000" dia="54." exitDia="0." initWt="1740." len="708.66" mDiv="10" mFix="1" mStep="-1." massFrac="39.66" mfg="Aerotech" peakThrust="656.223" propWt="690." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="354.33" f="0." m="690." t="0."/>\r
+<eng-data cg="354.33" f="440.418" m="688.164" t="0.015456"/>\r
+<eng-data cg="354.33" f="550.523" m="665.444" t="0.100464"/>\r
+<eng-data cg="354.33" f="546.118" m="638.014" t="0.193199"/>\r
+<eng-data cg="354.33" f="656.223" m="602.928" t="0.301391"/>\r
+<eng-data cg="354.33" f="647.414" m="532.279" t="0.502318"/>\r
+<eng-data cg="354.33" f="581.352" m="376.045" t="0.973725"/>\r
+<eng-data cg="354.33" f="471.247" m="231.241" t="1.48377"/>\r
+<eng-data cg="354.33" f="378.759" m="116.078" t="1.98609"/>\r
+<eng-data cg="354.33" f="334.718" m="78.8991" t="2.17929"/>\r
+<eng-data cg="354.33" f="255.442" m="59.2169" t="2.30294"/>\r
+<eng-data cg="354.33" f="158.55" m="37.6439" t="2.49614"/>\r
+<eng-data cg="354.33" f="57.2543" m="7.50646" t="3.01391"/>\r
+<eng-data cg="354.33" f="0." m="0." t="3.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+; Input by Tim Van Milligan using ThrustCurve Tracer by John Coker. Data from\r
+; Tripoli certification paperwork dated 25 November 2007.\r
+J401FJ 54 325 6 0.511 0.912 Aerotech\r
+ 0.011 440.414\r
+ 0.022 488.102\r
+ 0.075 427.791\r
+ 0.116 422.18\r
+ 0.191 446.024\r
+ 0.277 453.037\r
+ 0.382 462.855\r
+ 0.513 468.466\r
+ 0.712 472.673\r
+ 0.775 471.271\r
+ 0.948 471.271\r
+ 1.06 472.673\r
+ 1.281 469.868\r
+ 1.431 462.855\r
+ 1.607 453.037\r
+ 1.858 426.388\r
+ 2.034 403.946\r
+ 2.135 384.31\r
+ 2.202 378.7\r
+ 2.258 374.492\r
+ 2.277 374.492\r
+ 2.3 380.102\r
+ 2.322 380.102\r
+ 2.345 370.284\r
+ 2.367 359.064\r
+ 2.408 314.181\r
+ 2.461 244.051\r
+ 2.502 186.545\r
+ 2.566 103.792\r
+ 2.607 64.519\r
+ 2.652 42.078\r
+ 2.704 18.234\r
+ 2.783 0.0\r
+++ /dev/null
-; AeroTech J415W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J415W 54 314 0 0.686336 1.15718 AT\r
- 0.065 431.300\r
- 0.196 452.427\r
- 0.327 489.904\r
- 0.458 513.542\r
- 0.591 523.192\r
- 0.723 531.440\r
- 0.854 542.165\r
- 0.985 542.731\r
- 1.118 549.788\r
- 1.250 553.889\r
- 1.381 537.331\r
- 1.512 512.126\r
- 1.645 517.338\r
- 1.777 498.098\r
- 1.908 473.365\r
- 2.040 444.157\r
- 2.172 413.187\r
- 2.304 384.854\r
- 2.435 360.556\r
- 2.567 297.571\r
- 2.699 178.288\r
- 2.831 89.889\r
- 2.962 43.066\r
- 3.094 19.126\r
- 3.226 8.995\r
- 3.358 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="185.52" Itot="1201.33" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="343.236" burn-time="3.5" cgDiv="10" cgFix="1" cgStep="-1." code="J415W" delays="6,10,14" dia="54." exitDia="0." initWt="1198.9" len="326." mDiv="10" mFix="1" mStep="-1." massFrac="55.08" mfg="Aerotech" peakThrust="552." propWt="660.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="163." f="0." m="660.3" t="0."/>\r
+<eng-data cg="163." f="552." m="660.3" t="0."/>\r
+<eng-data cg="163." f="441.51" m="632.996" t="0.1"/>\r
+<eng-data cg="163." f="463.57" m="583.249" t="0.3"/>\r
+<eng-data cg="163." f="441.51" m="533.502" t="0.5"/>\r
+<eng-data cg="163." f="441.51" m="363.631" t="1.2"/>\r
+<eng-data cg="163." f="450.27" m="314.615" t="1.4"/>\r
+<eng-data cg="163." f="432.66" m="241.821" t="1.7"/>\r
+<eng-data cg="163." f="353.22" m="133.833" t="2.2"/>\r
+<eng-data cg="163." f="264.88" m="48.8992" t="2.7"/>\r
+<eng-data cg="163." f="220.75" m="35.5531" t="2.8"/>\r
+<eng-data cg="163." f="136.91" m="15.8946" t="3."/>\r
+<eng-data cg="163." f="88.29" m="9.70559" t="3.1"/>\r
+<eng-data cg="163." f="0." m="0." t="3.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech J420R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J420R 38 337 0 0.37632 0.6496 AT\r
- 0.031 61.083\r
- 0.095 563.470\r
- 0.160 525.283\r
- 0.224 521.242\r
- 0.288 527.371\r
- 0.352 537.088\r
- 0.418 535.138\r
- 0.481 534.623\r
- 0.545 530.245\r
- 0.610 526.447\r
- 0.674 517.203\r
- 0.738 510.279\r
- 0.802 500.887\r
- 0.868 479.450\r
- 0.931 460.675\r
- 0.995 438.594\r
- 1.060 409.647\r
- 1.124 383.454\r
- 1.188 361.024\r
- 1.252 339.741\r
- 1.318 319.194\r
- 1.381 296.714\r
- 1.445 195.191\r
- 1.510 61.984\r
- 1.575 7.220\r
- 1.640 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="174.23" Itot="650.979" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="404.335" burn-time="1.61" cgDiv="10" cgFix="1" cgStep="-1." code="J420R" delays="6,10,14" dia="38." exitDia="0." initWt="659." len="337." mDiv="10" mFix="1" mStep="-1." massFrac="57.81" mfg="Aerotech" peakThrust="563.47" propWt="381." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="168.5" f="0." m="381." t="0."/>\r
+<eng-data cg="168.5" f="61.08" m="380.464" t="0.03"/>\r
+<eng-data cg="168.5" f="563.47" m="367.67" t="0.1"/>\r
+<eng-data cg="168.5" f="525.28" m="348.554" t="0.16"/>\r
+<eng-data cg="168.5" f="521.24" m="330.179" t="0.22"/>\r
+<eng-data cg="168.5" f="527.37" m="308.698" t="0.29"/>\r
+<eng-data cg="168.5" f="537.09" m="290.008" t="0.35"/>\r
+<eng-data cg="168.5" f="535.14" m="268.044" t="0.42"/>\r
+<eng-data cg="168.5" f="534.62" m="249.261" t="0.48"/>\r
+<eng-data cg="168.5" f="530.25" m="227.448" t="0.55"/>\r
+<eng-data cg="168.5" f="526.45" m="208.894" t="0.61"/>\r
+<eng-data cg="168.5" f="517.2" m="190.57" t="0.67"/>\r
+<eng-data cg="168.5" f="510.28" m="169.522" t="0.74"/>\r
+<eng-data cg="168.5" f="500.89" m="151.768" t="0.8"/>\r
+<eng-data cg="168.5" f="479.45" m="131.686" t="0.87"/>\r
+<eng-data cg="168.5" f="460.68" m="115.179" t="0.93"/>\r
+<eng-data cg="168.5" f="438.59" m="96.7578" t="1."/>\r
+<eng-data cg="168.5" f="409.65" m="81.8643" t="1.06"/>\r
+<eng-data cg="168.5" f="383.45" m="67.9389" t="1.12"/>\r
+<eng-data cg="168.5" f="361.02" m="52.6887" t="1.19"/>\r
+<eng-data cg="168.5" f="339.74" m="40.3847" t="1.25"/>\r
+<eng-data cg="168.5" f="319.19" m="26.8868" t="1.32"/>\r
+<eng-data cg="168.5" f="296.71" m="16.0727" t="1.38"/>\r
+<eng-data cg="168.5" f="195.19" m="5.99635" t="1.45"/>\r
+<eng-data cg="168.5" f="61.98" m="1.48092" t="1.51"/>\r
+<eng-data cg="168.5" f="7.22" m="0.063385" t="1.58"/>\r
+<eng-data cg="168.5" f="0." m="0." t="1.61"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech J460T\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J460T 54 230 0 0.413504 0.801024 AT\r
- 0.041 500.927\r
- 0.125 509.423\r
- 0.209 516.357\r
- 0.294 527.752\r
- 0.379 535.135\r
- 0.464 541.858\r
- 0.548 545.793\r
- 0.633 545.678\r
- 0.718 544.832\r
- 0.802 540.278\r
- 0.887 533.698\r
- 0.972 526.340\r
- 1.056 511.003\r
- 1.141 492.475\r
- 1.225 474.977\r
- 1.310 457.021\r
- 1.395 437.203\r
- 1.479 418.093\r
- 1.565 403.240\r
- 1.649 339.173\r
- 1.733 203.861\r
- 1.819 102.620\r
- 1.903 49.295\r
- 1.987 9.538\r
- 2.073 2.155\r
- 2.158 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="212.38" Itot="812.671" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="427.721" burn-time="1.9" cgDiv="10" cgFix="1" cgStep="-1." code="J460T" delays="6,10,14" dia="54." exitDia="0." initWt="832.9" len="241." mDiv="10" mFix="1" mStep="-1." massFrac="46.85" mfg="Aerotech" peakThrust="582.91" propWt="390.2" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="120.5" f="0." m="390.2" t="0."/>\r
+<eng-data cg="120.5" f="582.91" m="390.2" t="0."/>\r
+<eng-data cg="120.5" f="515.43" m="363.832" t="0.1"/>\r
+<eng-data cg="120.5" f="510.85" m="339.194" t="0.2"/>\r
+<eng-data cg="120.5" f="506.36" m="241.512" t="0.6"/>\r
+<eng-data cg="120.5" f="492.93" m="169.541" t="0.9"/>\r
+<eng-data cg="120.5" f="448.09" m="79.176" t="1.3"/>\r
+<eng-data cg="120.5" f="412.24" m="37.8676" t="1.5"/>\r
+<eng-data cg="120.5" f="336.05" m="19.9032" t="1.6"/>\r
+<eng-data cg="120.5" f="179.25" m="7.53228" t="1.7"/>\r
+<eng-data cg="120.5" f="67.25" m="1.61449" t="1.8"/>\r
+<eng-data cg="120.5" f="0." m="0." t="1.9"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;Delays are speculation.\r
-;Taken from Aerotech curves, not cert docs.\r
-;Jim Yehle 15 Nov 07\r
-J500G 38 335.407 0-6-10-14 0.3626 0.654 Aerotech \r
-0.0134378 40.2458\r
-0.0335946 724.425\r
-0.0403135 781.616\r
-0.0604703 787.971\r
-0.0895857 711.716\r
-0.134378 686.297\r
-0.394177 637.578\r
-0.575588 588.86\r
-0.606943 622.751\r
-0.633819 620.633\r
-1.20045 360.094\r
-1.24076 345.267\r
-1.31019 182.165\r
-1.38186 65.6642\r
-1.43337 23.3002\r
-1.45 0\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Aerotech" code="J500G" Type="reloadable" dia="38." len="335.407"\r
+initWt="654." propWt="362.6" delays="0,6,10,14" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="498.389" peakThrust="787.971" throatDia="0."\r
+exitDia="0." Itot="722.664" burn-time="1.45" massFrac="55.44" Isp="203.23"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Delays are speculation.\r
+Taken from Aerotech curves, not cert docs.\r
+Jim Yehle 15 Nov 07</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="362.6" cg="167.703"/>\r
+ <eng-data t="0.0134378" f="40.2458" m="362.464" cg="167.703"/>\r
+ <eng-data t="0.0335946" f="724.425" m="358.597" cg="167.703"/>\r
+ <eng-data t="0.0403135" f="781.616" m="356.059" cg="167.703"/>\r
+ <eng-data t="0.0604703" f="787.971" m="348.122" cg="167.703"/>\r
+ <eng-data t="0.0895857" f="711.716" m="337.167" cg="167.703"/>\r
+ <eng-data t="0.134378" f="686.297" m="321.457" cg="167.703"/>\r
+ <eng-data t="0.394177" f="637.578" m="235.17" cg="167.703"/>\r
+ <eng-data t="0.575588" f="588.86" m="179.353" cg="167.703"/>\r
+ <eng-data t="0.606943" f="622.751" m="169.822" cg="167.703"/>\r
+ <eng-data t="0.633819" f="620.633" m="161.438" cg="167.703"/>\r
+ <eng-data t="1.20045" f="360.094" m="22.0236" cg="167.703"/>\r
+ <eng-data t="1.24076" f="345.267" m="14.8898" cg="167.703"/>\r
+ <eng-data t="1.31019" f="182.165" m="5.70288" cg="167.703"/>\r
+ <eng-data t="1.38186" f="65.6642" m="1.24691" cg="167.703"/>\r
+ <eng-data t="1.43337" f="23.3002" m="0.0972067" cg="167.703"/>\r
+ <eng-data t="1.45" f="0." m="0." cg="167.703"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+J510 38 584 P 0.662 1.08 AT\r
+ 0.032 1055.904\r
+ 0.11 865.54\r
+ 0.161 829.933\r
+ 0.267 794.325\r
+ 0.351 780.63\r
+ 0.512 705.306\r
+ 0.682 654.633\r
+ 1.318 624.504\r
+ 1.461 475.225\r
+ 1.623 345.121\r
+ 1.934 153.387\r
+ 2.039 115.04\r
+ 2.177 41.086\r
+ 2.317 5.478\r
+ 2.5 0.0\r
+++ /dev/null
-; AeroTech J540R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J540R 54 314 0 0.61376 1.08416 AT\r
- 0.044 498.757\r
- 0.134 639.617\r
- 0.224 649.317\r
- 0.314 657.966\r
- 0.404 664.020\r
- 0.494 666.924\r
- 0.584 663.699\r
- 0.675 658.398\r
- 0.765 651.232\r
- 0.855 638.505\r
- 0.945 626.396\r
- 1.035 612.557\r
- 1.126 590.090\r
- 1.216 562.391\r
- 1.306 536.875\r
- 1.396 511.607\r
- 1.486 490.354\r
- 1.576 468.978\r
- 1.667 451.342\r
- 1.758 430.180\r
- 1.847 414.549\r
- 1.937 398.116\r
- 2.027 305.877\r
- 2.118 55.541\r
- 2.208 1.523\r
- 2.299 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="188.79" Itot="1149.7" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="510.979" burn-time="2.25" cgDiv="10" cgFix="1" cgStep="-1." code="J540R" delays="6,10,14,1000" dia="54." exitDia="0." initWt="1100." len="314." mDiv="10" mFix="1" mStep="-1." massFrac="56.45" mfg="Aerotech" peakThrust="666.92" propWt="621." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="157." f="0." m="621." t="0."/>\r
+<eng-data cg="157." f="498.76" m="615.612" t="0.04"/>\r
+<eng-data cg="157." f="639.62" m="587.942" t="0.13"/>\r
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+<eng-data cg="157." f="590.09" m="239.269" t="1.13"/>\r
+<eng-data cg="157." f="562.39" m="211.257" t="1.22"/>\r
+<eng-data cg="157." f="536.88" m="184.537" t="1.31"/>\r
+<eng-data cg="157." f="511.61" m="159.053" t="1.4"/>\r
+<eng-data cg="157." f="490.35" m="134.699" t="1.49"/>\r
+<eng-data cg="157." f="468.98" m="111.381" t="1.58"/>\r
+<eng-data cg="157." f="451.34" m="89.0114" t="1.67"/>\r
+<eng-data cg="157." f="430.18" m="67.5849" t="1.76"/>\r
+<eng-data cg="157." f="414.55" m="47.0527" t="1.85"/>\r
+<eng-data cg="157." f="398.12" m="27.2997" t="1.94"/>\r
+<eng-data cg="157." f="305.88" m="10.1881" t="2.03"/>\r
+<eng-data cg="157." f="55.54" m="1.40334" t="2.12"/>\r
+<eng-data cg="157." f="1.52" m="0.0164202" t="2.21"/>\r
+<eng-data cg="157." f="0." m="0." t="2.25"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech J570W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J570W 38 479 0 0.547904 0.886144 AT\r
- 0.039 1149.795\r
- 0.119 1042.846\r
- 0.199 960.891\r
- 0.279 900.020\r
- 0.360 837.772\r
- 0.441 792.834\r
- 0.521 735.510\r
- 0.602 685.857\r
- 0.682 649.599\r
- 0.762 608.757\r
- 0.844 597.350\r
- 0.924 568.934\r
- 1.004 548.552\r
- 1.084 505.080\r
- 1.165 484.626\r
- 1.246 452.328\r
- 1.326 362.439\r
- 1.406 297.973\r
- 1.487 262.381\r
- 1.568 195.696\r
- 1.648 156.733\r
- 1.729 124.649\r
- 1.809 113.749\r
- 1.890 69.812\r
- 1.971 46.023\r
- 2.052 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="192.41" Itot="1033.83" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="503.817" burn-time="2.05" cgDiv="10" cgFix="1" cgStep="-1." code="J570W" delays="6,10,14" dia="38." exitDia="0." initWt="886.144" len="479." mDiv="10" mFix="1" mStep="-1." massFrac="61.83" mfg="Aerotech" peakThrust="1149.8" propWt="547.904" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="239.5" f="0." m="547.904" t="0."/>\r
+<eng-data cg="239.5" f="1149.8" m="536.021" t="0.039"/>\r
+<eng-data cg="239.5" f="1042.85" m="489.54" t="0.119"/>\r
+<eng-data cg="239.5" f="960.891" m="447.062" t="0.199"/>\r
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+<eng-data cg="239.5" f="649.599" m="244.096" t="0.682"/>\r
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+<eng-data cg="239.5" f="548.552" m="142.8" t="1.004"/>\r
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+<eng-data cg="239.5" f="452.328" m="79.1102" t="1.246"/>\r
+<eng-data cg="239.5" f="362.439" m="61.8381" t="1.326"/>\r
+<eng-data cg="239.5" f="297.973" m="47.838" t="1.406"/>\r
+<eng-data cg="239.5" f="262.381" m="35.8106" t="1.487"/>\r
+<eng-data cg="239.5" f="195.696" m="25.9785" t="1.568"/>\r
+<eng-data cg="239.5" f="156.733" m="18.5074" t="1.648"/>\r
+<eng-data cg="239.5" f="124.649" m="12.4678" t="1.729"/>\r
+<eng-data cg="239.5" f="113.749" m="7.41405" t="1.809"/>\r
+<eng-data cg="239.5" f="69.812" m="3.47411" t="1.89"/>\r
+<eng-data cg="239.5" f="46.023" m="0.987834" t="1.971"/>\r
+<eng-data cg="239.5" f="0." m="0." t="2.052"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-J575FJ 38 478.79 6-10-14 0.576 0.91424 Aerotech \r
-0.0156556 656.682\r
-0.0195695 840.689\r
-0.037182 840.689\r
-0.0606654 839.001\r
-0.101761 839.001\r
-0.162427 839.001\r
-0.228963 839.001\r
-0.315068 839.001\r
-0.399217 837.312\r
-0.459883 837.312\r
-0.547945 822.119\r
-0.60274 801.862\r
-0.700587 742.777\r
-0.802348 685.381\r
-0.841487 646.554\r
-0.902153 573.964\r
-0.949791 483.69\r
-1 319.581\r
-1.05365 220.66\r
-1.12916 153.62\r
-1.19961 99.5997\r
-1.27593 43.8914\r
-1.34 0\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Aerotech" code="J575FJ" Type="reloadable" dia="38." len="478.79"\r
+initWt="914.24" propWt="576." delays="6,10,14" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="597.435" peakThrust="884.242" throatDia="0."\r
+exitDia="0." Itot="800.563" burn-time="1.34" massFrac="63." Isp="141.73"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="576." cg="239.4"/>\r
+ <eng-data t="0.0156556" f="656.682" m="572.302" cg="239.4"/>\r
+ <eng-data t="0.0195695" f="840.689" m="570.193" cg="239.4"/>\r
+ <eng-data t="0.0550206" f="878.839" m="548.263" cg="239.4"/>\r
+ <eng-data t="0.090784" f="880.64" m="525.626" cg="239.4"/>\r
+ <eng-data t="0.154058" f="882.441" m="485.494" cg="239.4"/>\r
+ <eng-data t="0.209078" f="884.242" m="450.525" cg="239.4"/>\r
+ <eng-data t="0.261348" f="880.64" m="417.339" cg="239.4"/>\r
+ <eng-data t="0.341128" f="878.839" m="366.841" cg="239.4"/>\r
+ <eng-data t="0.390646" f="873.436" m="335.625" cg="239.4"/>\r
+ <eng-data t="0.451169" f="862.631" m="297.826" cg="239.4"/>\r
+ <eng-data t="0.525447" f="821.21" m="252.832" cg="239.4"/>\r
+ <eng-data t="0.599725" f="783.391" m="209.955" cg="239.4"/>\r
+ <eng-data t="0.797799" f="669.935" m="106.396" cg="239.4"/>\r
+ <eng-data t="0.836314" f="639.319" m="88.2555" cg="239.4"/>\r
+ <eng-data t="1.00138" f="340.37" m="30.0811" cg="239.4"/>\r
+ <eng-data t="1.0729" f="205.303" m="16.0401" cg="239.4"/>\r
+ <eng-data t="1.14993" f="108.054" m="7.35668" cg="239.4"/>\r
+ <eng-data t="1.21045" f="72.036" m="3.43561" cg="239.4"/>\r
+ <eng-data t="1.28473" f="32.4162" m="0.644517" cg="239.4"/>\r
+ <eng-data t="1.34" f="0." m="0." cg="239.4"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech J800T\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J800T 54 314 0 0.613312 1.08595 AT\r
- 0.040 841.341\r
- 0.121 818.497\r
- 0.203 776.386\r
- 0.285 784.308\r
- 0.367 785.314\r
- 0.449 783.315\r
- 0.531 782.539\r
- 0.612 779.977\r
- 0.695 773.680\r
- 0.777 765.307\r
- 0.858 755.517\r
- 0.941 744.777\r
- 1.023 733.131\r
- 1.105 719.947\r
- 1.187 702.235\r
- 1.269 685.369\r
- 1.351 668.265\r
- 1.433 650.327\r
- 1.515 630.472\r
- 1.597 615.483\r
- 1.679 470.262\r
- 1.760 256.617\r
- 1.843 108.716\r
- 1.925 15.005\r
- 2.007 1.249\r
- 2.090 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="216.65" Itot="1264.8" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="790.502" burn-time="1.6" cgDiv="10" cgFix="1" cgStep="-1." code="J800T" delays="6,10,14,18" dia="54." exitDia="0." initWt="1133.9" len="326." mDiv="10" mFix="1" mStep="-1." massFrac="52.5" mfg="Aerotech" peakThrust="1255.67" propWt="595.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="163." f="0." m="595.3" t="0."/>\r
+<eng-data cg="163." f="1255.67" m="595.3" t="0."/>\r
+<eng-data cg="163." f="1102.7" m="539.8" t="0.1"/>\r
+<eng-data cg="163." f="1067.83" m="488.72" t="0.2"/>\r
+<eng-data cg="163." f="1045.99" m="438.975" t="0.3"/>\r
+<eng-data cg="163." f="1002.4" m="294.359" t="0.6"/>\r
+<eng-data cg="163." f="971.89" m="247.897" t="0.7"/>\r
+<eng-data cg="163." f="937.02" m="202.974" t="0.8"/>\r
+<eng-data cg="163." f="841.12" m="161.128" t="0.9"/>\r
+<eng-data cg="163." f="588.38" m="26.5649" t="1.3"/>\r
+<eng-data cg="163." f="217.91" m="7.5902" t="1.4"/>\r
+<eng-data cg="163." f="52.31" m="1.23103" t="1.5"/>\r
+<eng-data cg="163." f="0." m="0." t="1.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Aerotech" code="J825R-M" Type="reloadable" dia="38." len="478.282"\r
+initWt="875." propWt="497." delays="0" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="677.424" peakThrust="1069.87" throatDia="0." exitDia="0."\r
+Itot="929.355" burn-time="1.37" massFrac="56.8" Isp="190.68" tDiv="15"\r
+tStep="-1." tFix="1" FDiv="6" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1"\r
+cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="497." cg="239.141"/>\r
+ <eng-data t="0." f="11.504" m="497." cg="239.141"/>\r
+ <eng-data t="0.048913" f="1069.87" m="482.857" cg="239.141"/>\r
+ <eng-data t="0.100155" f="977.842" m="454.8" cg="239.141"/>\r
+ <eng-data t="0.118789" f="1035.36" m="444.769" cg="239.141"/>\r
+ <eng-data t="0.652174" f="897.314" m="169.128" cg="239.141"/>\r
+ <eng-data t="0.801242" f="839.794" m="99.8879" cg="239.141"/>\r
+ <eng-data t="0.899068" f="782.274" m="57.4583" cg="239.141"/>\r
+ <eng-data t="0.999224" f="586.705" m="20.7964" cg="239.141"/>\r
+ <eng-data t="1.09938" f="103.536" m="2.31144" cg="239.141"/>\r
+ <eng-data t="1.14363" f="23.008" m="0.814008" cg="239.141"/>\r
+ <eng-data t="1.18" f="0." m="0.590278" cg="239.141"/>\r
+ <eng-data t="1.37189" f="11.504" m="0." cg="239.141"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech J90W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J90W 54 243 0 0.427392 0.852544 AT\r
- 0.143 116.187\r
- 0.430 165.444\r
- 0.718 176.536\r
- 1.005 184.645\r
- 1.293 187.242\r
- 1.580 183.651\r
- 1.868 175.492\r
- 2.155 167.687\r
- 2.443 156.858\r
- 2.730 143.514\r
- 3.018 128.856\r
- 3.305 110.879\r
- 3.593 94.003\r
- 3.880 79.657\r
- 4.168 67.472\r
- 4.455 57.268\r
- 4.743 48.008\r
- 5.030 40.523\r
- 5.318 33.901\r
- 5.605 28.248\r
- 5.893 23.334\r
- 6.180 19.275\r
- 6.468 15.923\r
- 6.755 12.727\r
- 7.044 9.903\r
- 7.332 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="193.24" Itot="741.715" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="98.895" burn-time="7.5" cgDiv="10" cgFix="1" cgStep="-1." code="J90W" delays="6,10,14" dia="54." exitDia="0." initWt="834.1" len="241." mDiv="10" mFix="1" mStep="-1." massFrac="46.92" mfg="Aerotech" peakThrust="173.83" propWt="391.4" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="120.5" f="0." m="391.4" t="0."/>\r
+<eng-data cg="120.5" f="120.9" m="391.4" t="0."/>\r
+<eng-data cg="120.5" f="155.5" m="318.472" t="1."/>\r
+<eng-data cg="120.5" f="173.83" m="231.579" t="2."/>\r
+<eng-data cg="120.5" f="173.34" m="185.779" t="2.5"/>\r
+<eng-data cg="120.5" f="163.73" m="141.312" t="3."/>\r
+<eng-data cg="120.5" f="142.69" m="100.888" t="3.5"/>\r
+<eng-data cg="120.5" f="107.51" m="67.8802" t="4."/>\r
+<eng-data cg="120.5" f="54.44" m="25.15" t="5."/>\r
+<eng-data cg="120.5" f="34.74" m="13.385" t="5.5"/>\r
+<eng-data cg="120.5" f="19.66" m="6.20834" t="6."/>\r
+<eng-data cg="120.5" f="10.05" m="2.28888" t="6.5"/>\r
+<eng-data cg="120.5" f="3.65" m="0.481523" t="7."/>\r
+<eng-data cg="120.5" f="0." m="0." t="7.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+J99 54 231 P 0.556 0.899 AT\r
+ 0.031 117.296\r
+ 0.078 135.045\r
+ 0.242 144.305\r
+ 0.828 131.38\r
+ 2.539 110.737\r
+ 3.594 102.056\r
+ 4.82 94.146\r
+ 5.938 86.043\r
+ 7.523 81.22\r
+ 8.984 76.976\r
+ 9.047 74.082\r
+ 9.547 16.012\r
+ 9.711 5.209\r
+ 9.82 1.929\r
+ 10.0 0.0\r
+++ /dev/null
-; AeroTech K1050W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-K1050W 54 676 0 1.34714 2.12845 AT\r
- 0.049 1305.649\r
- 0.149 1270.386\r
- 0.249 1288.922\r
- 0.349 1327.059\r
- 0.449 1345.719\r
- 0.549 1359.794\r
- 0.649 1364.452\r
- 0.749 1365.493\r
- 0.849 1377.189\r
- 0.949 1379.519\r
- 1.049 1346.586\r
- 1.149 1286.742\r
- 1.249 1232.101\r
- 1.349 1186.480\r
- 1.449 1156.521\r
- 1.549 1120.045\r
- 1.649 1098.708\r
- 1.749 1070.186\r
- 1.849 889.885\r
- 1.949 646.691\r
- 2.049 441.213\r
- 2.149 302.245\r
- 2.249 155.001\r
- 2.349 52.187\r
- 2.449 43.415\r
- 2.549 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="187.31" Itot="2522.04" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1025.22" burn-time="2.46" cgDiv="10" cgFix="1" cgStep="-1." code="K1050W" delays="1000" dia="54." exitDia="0." initWt="2259." len="635." mDiv="10" mFix="1" mStep="-1." massFrac="60.78" mfg="Aerotech" peakThrust="1468.5" propWt="1373." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="317.5" f="0." m="1373." t="0."/>\r
+<eng-data cg="317.5" f="934.5" m="1373." t="0."/>\r
+<eng-data cg="317.5" f="1468.5" m="1340.3" t="0.05"/>\r
+<eng-data cg="317.5" f="1335." m="1302.14" t="0.1"/>\r
+<eng-data cg="317.5" f="1290.5" m="1266.41" t="0.15"/>\r
+<eng-data cg="317.5" f="1246." m="1197.36" t="0.25"/>\r
+<eng-data cg="317.5" f="1246." m="858.201" t="0.75"/>\r
+<eng-data cg="317.5" f="1201.5" m="525.095" t="1.25"/>\r
+<eng-data cg="317.5" f="1157." m="364.599" t="1.5"/>\r
+<eng-data cg="317.5" f="1157." m="270.118" t="1.65"/>\r
+<eng-data cg="317.5" f="1246." m="204.708" t="1.75"/>\r
+<eng-data cg="317.5" f="890." m="117.495" t="1.9"/>\r
+<eng-data cg="317.5" f="578.5" m="37.5501" t="2.1"/>\r
+<eng-data cg="317.5" f="222.5" m="15.7468" t="2.2"/>\r
+<eng-data cg="317.5" f="0." m="0." t="2.46"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech K1100T\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-K1100T 54 398 0 0.7616 1.32518 AT\r
- 0.034 1234.653\r
- 0.105 1233.429\r
- 0.176 1192.393\r
- 0.247 1163.041\r
- 0.318 1147.963\r
- 0.389 1146.319\r
- 0.460 1140.958\r
- 0.532 1132.640\r
- 0.603 1123.824\r
- 0.674 1108.921\r
- 0.745 1090.974\r
- 0.816 1073.937\r
- 0.887 1049.133\r
- 0.959 1021.216\r
- 1.030 994.559\r
- 1.101 966.571\r
- 1.172 940.194\r
- 1.243 909.792\r
- 1.315 880.264\r
- 1.386 844.477\r
- 1.457 643.599\r
- 1.528 401.861\r
- 1.599 145.498\r
- 1.670 28.372\r
- 1.742 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="208.59" Itot="1618.86" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1011.78" burn-time="1.6" cgDiv="10" cgFix="1" cgStep="-1." code="K1100T" delays="6,10,14,18" dia="54." exitDia="0." initWt="1426.1" len="410." mDiv="10" mFix="1" mStep="-1." massFrac="55.49" mfg="Aerotech" peakThrust="1627.57" propWt="791.4" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="205." f="0." m="791.4" t="0."/>\r
+<eng-data cg="205." f="1627.57" m="791.4" t="0."/>\r
+<eng-data cg="205." f="1244.55" m="721.196" t="0.1"/>\r
+<eng-data cg="205." f="1196.65" m="542.184" t="0.4"/>\r
+<eng-data cg="205." f="1124.9" m="315.2" t="0.8"/>\r
+<eng-data cg="205." f="1077.04" m="207.555" t="1."/>\r
+<eng-data cg="205." f="1053.06" m="155.488" t="1.1"/>\r
+<eng-data cg="205." f="1029.09" m="104.594" t="1.2"/>\r
+<eng-data cg="205." f="660.53" m="21.9947" t="1.4"/>\r
+<eng-data cg="205." f="119.65" m="2.92463" t="1.5"/>\r
+<eng-data cg="205." f="0." m="0." t="1.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="166.23" Itot="2132.31" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1066.15" burn-time="2." cgDiv="10" cgFix="1" cgStep="-1." code="K1275" delays="1000" dia="54." exitDia="0." initWt="2061." len="569." mDiv="10" mFix="1" mStep="-1." massFrac="63.46" mfg="Aerotech" peakThrust="1557.99" propWt="1308." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="284.5" f="0." m="1308." t="0."/>\r
+<eng-data cg="284.5" f="1282.62" m="1292.26" t="0.04"/>\r
+<eng-data cg="284.5" f="1557.99" m="1222.56" t="0.12"/>\r
+<eng-data cg="284.5" f="1540.2" m="1146.55" t="0.2"/>\r
+<eng-data cg="284.5" f="1526.78" m="1071.29" t="0.28"/>\r
+<eng-data cg="284.5" f="1500.69" m="997.007" t="0.36"/>\r
+<eng-data cg="284.5" f="1456.58" m="924.445" t="0.44"/>\r
+<eng-data cg="284.5" f="1425.79" m="853.721" t="0.52"/>\r
+<eng-data cg="284.5" f="1390.42" m="784.62" t="0.6"/>\r
+<eng-data cg="284.5" f="1355.11" m="717.254" t="0.68"/>\r
+<eng-data cg="284.5" f="1323.31" m="651.534" t="0.76"/>\r
+<eng-data cg="284.5" f="1282.83" m="587.588" t="0.84"/>\r
+<eng-data cg="284.5" f="1247.8" m="525.494" t="0.92"/>\r
+<eng-data cg="284.5" f="1194.42" m="465.57" t="1."/>\r
+<eng-data cg="284.5" f="1150.98" m="408.022" t="1.08"/>\r
+<eng-data cg="284.5" f="1108.22" m="352.588" t="1.16"/>\r
+<eng-data cg="284.5" f="1068.75" m="299.172" t="1.24"/>\r
+<eng-data cg="284.5" f="1036.92" m="247.506" t="1.32"/>\r
+<eng-data cg="284.5" f="997.44" m="197.589" t="1.4"/>\r
+<eng-data cg="284.5" f="964.57" m="149.448" t="1.48"/>\r
+<eng-data cg="284.5" f="933.3" m="102.88" t="1.56"/>\r
+<eng-data cg="284.5" f="889.99" m="58.1426" t="1.64"/>\r
+<eng-data cg="284.5" f="599.47" m="21.596" t="1.72"/>\r
+<eng-data cg="284.5" f="134.56" m="3.58531" t="1.8"/>\r
+<eng-data cg="284.5" f="5.63" m="0.145503" t="1.88"/>\r
+<eng-data cg="284.5" f="0.2" m="0.00245368" t="1.96"/>\r
+<eng-data cg="284.5" f="0." m="0." t="2."/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;Entered by Jim Yehle\r
-;from TRA cert document\r
-K1499N 75 260 1000 0.604 1.741 AT-RMS \r
-0.01 1450\r
-0.2 1720.12\r
-0.35 1700\r
-0.5 1600\r
-0.6 1575\r
-0.7 1500\r
-0.82 1400\r
-0.84 250\r
-0.88 0\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="AT-RMS" code="K1499N" Type="reloadable" dia="75." len="260." initWt="1741."\r
+propWt="604." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="1499.8" peakThrust="1720.12" throatDia="0." exitDia="0." Itot="1321.7"\r
+burn-time="0.88" massFrac="0." Isp="223.1" tDiv="10" tStep="-1." tFix="1"\r
+FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+ <comments>Entered by Jim Yehle\r
+from TRA cert document</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="604." cg="130."/>\r
+ <eng-data t="0.01" f="1450." m="600.684" cg="130."/>\r
+ <eng-data t="0.2" f="1720.12" m="462.926" cg="130."/>\r
+ <eng-data t="0.35" f="1700." m="345.594" cg="130."/>\r
+ <eng-data t="0.5" f="1600." m="232.378" cg="130."/>\r
+ <eng-data t="0.6" f="1575." m="159.76" cg="130."/>\r
+ <eng-data t="0.7" f="1500." m="89.429" cg="130."/>\r
+ <eng-data t="0.82" f="1400." m="9.8349" cg="130."/>\r
+ <eng-data t="0.84" f="250." m="2.28719" cg="130."/>\r
+ <eng-data t="0.88" f="0." m="0." cg="130."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech K185W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-K185W 54 437 0 0.827008 1.43405 AT\r
- 0.150 279.128\r
- 0.452 308.220\r
- 0.754 328.435\r
- 1.056 338.929\r
- 1.359 339.677\r
- 1.663 333.166\r
- 1.965 321.891\r
- 2.267 309.687\r
- 2.570 293.260\r
- 2.873 271.536\r
- 3.175 247.174\r
- 3.477 216.883\r
- 3.780 186.951\r
- 4.083 161.096\r
- 4.385 138.113\r
- 4.688 117.749\r
- 4.991 99.372\r
- 5.294 82.759\r
- 5.596 68.426\r
- 5.898 55.126\r
- 6.201 44.162\r
- 6.504 34.209\r
- 6.806 25.064\r
- 7.108 16.880\r
- 7.411 9.200\r
- 7.715 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="169.98" Itot="1378.58" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="178.688" burn-time="7.71" cgDiv="10" cgFix="1" cgStep="-1." code="K185W" delays="1000" dia="54." exitDia="0." initWt="1434.05" len="437." mDiv="10" mFix="1" mStep="-1." massFrac="57.67" mfg="Aerotech" peakThrust="339.677" propWt="827.008" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AeroTech K185W\r
+Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
+provided by ThrustCurve.org (www.thrustcurve.org)\r
+</comments>\r
+<data>\r
+<eng-data cg="218.5" f="0." m="827.008" t="0."/>\r
+<eng-data cg="218.5" f="279.128" m="814.449" t="0.15"/>\r
+<eng-data cg="218.5" f="308.22" m="761.245" t="0.452"/>\r
+<eng-data cg="218.5" f="328.435" m="703.573" t="0.754"/>\r
+<eng-data cg="218.5" f="338.929" m="643.12" t="1.056"/>\r
+<eng-data cg="218.5" f="339.677" m="581.445" t="1.359"/>\r
+<eng-data cg="218.5" f="333.166" m="520.093" t="1.663"/>\r
+<eng-data cg="218.5" f="321.891" m="460.754" t="1.965"/>\r
+<eng-data cg="218.5" f="309.687" m="403.543" t="2.267"/>\r
+<eng-data cg="218.5" f="293.26" m="348.744" t="2.57"/>\r
+<eng-data cg="218.5" f="271.536" m="297.413" t="2.873"/>\r
+<eng-data cg="218.5" f="247.174" m="250.426" t="3.175"/>\r
+<eng-data cg="218.5" f="216.883" m="208.389" t="3.477"/>\r
+<eng-data cg="218.5" f="186.951" m="171.687" t="3.78"/>\r
+<eng-data cg="218.5" f="161.096" m="140.055" t="4.083"/>\r
+<eng-data cg="218.5" f="138.113" m="112.951" t="4.385"/>\r
+<eng-data cg="218.5" f="117.749" m="89.6972" t="4.688"/>\r
+<eng-data cg="218.5" f="99.372" m="69.9643" t="4.991"/>\r
+<eng-data cg="218.5" f="82.759" m="53.4113" t="5.294"/>\r
+<eng-data cg="218.5" f="68.426" m="39.7163" t="5.596"/>\r
+<eng-data cg="218.5" f="55.126" m="28.5244" t="5.898"/>\r
+<eng-data cg="218.5" f="44.162" m="19.5006" t="6.201"/>\r
+<eng-data cg="218.5" f="34.209" m="12.3779" t="6.504"/>\r
+<eng-data cg="218.5" f="25.064" m="7.00866" t="6.806"/>\r
+<eng-data cg="218.5" f="16.88" m="3.20917" t="7.108"/>\r
+<eng-data cg="218.5" f="9.2" m="0.838899" t="7.411"/>\r
+<eng-data cg="218.5" f="0." m="0." t="7.715"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech K250W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-K250W 54 673 0 1.52902 2.21133 AT\r
- 0.199 365.330\r
- 0.599 403.324\r
- 0.999 418.669\r
- 1.400 409.813\r
- 1.801 408.949\r
- 2.201 412.146\r
- 2.602 411.952\r
- 3.003 409.488\r
- 3.403 393.214\r
- 3.804 373.599\r
- 4.205 348.913\r
- 4.605 328.463\r
- 5.006 307.163\r
- 5.407 281.467\r
- 5.807 249.011\r
- 6.208 217.159\r
- 6.609 185.908\r
- 7.009 149.190\r
- 7.410 119.808\r
- 7.811 92.096\r
- 8.211 69.726\r
- 8.613 52.613\r
- 9.014 35.876\r
- 9.414 16.727\r
- 9.815 4.086\r
- 10.216 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="170.26" Itot="2553.02" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="249.904" burn-time="10.22" cgDiv="10" cgFix="1" cgStep="-1." code="K250W" delays="1000" dia="54." exitDia="0." initWt="2211.33" len="673." mDiv="10" mFix="1" mStep="-1." massFrac="69.14" mfg="Aerotech" peakThrust="418.669" propWt="1529.02" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AeroTech K250W\r
+Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
+provided by ThrustCurve.org (www.thrustcurve.org)\r
+</comments>\r
+<data>\r
+<eng-data cg="336.5" f="0." m="1529.02" t="0."/>\r
+<eng-data cg="336.5" f="365.33" m="1507.25" t="0.199"/>\r
+<eng-data cg="336.5" f="403.324" m="1415.18" t="0.599"/>\r
+<eng-data cg="336.5" f="418.669" m="1316.72" t="0.999"/>\r
+<eng-data cg="336.5" f="409.813" m="1217.23" t="1.4"/>\r
+<eng-data cg="336.5" f="408.949" m="1118.92" t="1.801"/>\r
+<eng-data cg="336.5" f="412.146" m="1020.57" t="2.201"/>\r
+<eng-data cg="336.5" f="411.952" m="921.607" t="2.602"/>\r
+<eng-data cg="336.5" f="409.488" m="822.968" t="3.003"/>\r
+<eng-data cg="336.5" f="393.214" m="726.819" t="3.403"/>\r
+<eng-data cg="336.5" f="373.599" m="634.739" t="3.804"/>\r
+<eng-data cg="336.5" f="348.913" m="547.98" t="4.205"/>\r
+<eng-data cg="336.5" f="328.463" m="466.842" t="4.605"/>\r
+<eng-data cg="336.5" f="307.163" m="390.516" t="5.006"/>\r
+<eng-data cg="336.5" f="281.467" m="319.833" t="5.407"/>\r
+<eng-data cg="336.5" f="249.011" m="256.291" t="5.807"/>\r
+<eng-data cg="336.5" f="217.159" m="200.313" t="6.208"/>\r
+<eng-data cg="336.5" f="185.908" m="151.913" t="6.609"/>\r
+<eng-data cg="336.5" f="149.19" m="111.774" t="7.009"/>\r
+<eng-data cg="336.5" f="119.808" m="79.4727" t="7.41"/>\r
+<eng-data cg="336.5" f="92.096" m="54.0271" t="7.811"/>\r
+<eng-data cg="336.5" f="69.726" m="34.6438" t="8.211"/>\r
+<eng-data cg="336.5" f="52.613" m="19.9166" t="8.613"/>\r
+<eng-data cg="336.5" f="35.876" m="9.29075" t="9.014"/>\r
+<eng-data cg="336.5" f="16.727" m="2.98989" t="9.414"/>\r
+<eng-data cg="336.5" f="4.086" m="0.49065" t="9.815"/>\r
+<eng-data cg="336.5" f="0." m="0." t="10.216"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech K458W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-K458W 98 275 0 1.42778 3.16378 AT\r
- 0.133 294.911\r
- 0.403 404.808\r
- 0.674 462.021\r
- 0.944 515.863\r
- 1.214 555.072\r
- 1.484 583.153\r
- 1.755 600.299\r
- 2.025 610.254\r
- 2.295 618.543\r
- 2.566 623.155\r
- 2.835 618.885\r
- 3.105 589.082\r
- 3.376 546.307\r
- 3.647 505.042\r
- 3.917 451.412\r
- 4.186 391.651\r
- 4.457 338.409\r
- 4.727 288.429\r
- 4.997 245.814\r
- 5.268 208.209\r
- 5.539 178.153\r
- 5.808 149.825\r
- 6.078 62.931\r
- 6.349 8.427\r
- 6.620 2.562\r
- 6.891 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="196.28" Itot="2560.01" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="400.002" burn-time="6.4" cgDiv="10" cgFix="1" cgStep="-1." code="K458W" delays="1000" dia="98." exitDia="0." initWt="3106.2" len="275." mDiv="10" mFix="1" mStep="-1." massFrac="42.82" mfg="Aerotech" peakThrust="596.79" propWt="1330." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="137.5" f="0." m="1330." t="0."/>\r
+<eng-data cg="137.5" f="417.98" m="1330." t="0."/>\r
+<eng-data cg="137.5" f="358.91" m="1289.64" t="0.2"/>\r
+<eng-data cg="137.5" f="379.77" m="1251.26" t="0.4"/>\r
+<eng-data cg="137.5" f="404.81" m="1190.12" t="0.7"/>\r
+<eng-data cg="137.5" f="467.44" m="1076.83" t="1.2"/>\r
+<eng-data cg="137.5" f="538.39" m="893.935" t="1.9"/>\r
+<eng-data cg="137.5" f="596.79" m="687.52" t="2.6"/>\r
+<eng-data cg="137.5" f="538.39" m="392.641" t="3.6"/>\r
+<eng-data cg="137.5" f="500.8" m="365.646" t="3.7"/>\r
+<eng-data cg="137.5" f="313.01" m="175.387" t="4.6"/>\r
+<eng-data cg="137.5" f="287.96" m="144.165" t="4.8"/>\r
+<eng-data cg="137.5" f="166.89" m="26.0112" t="5.8"/>\r
+<eng-data cg="137.5" f="0." m="0." t="6.4"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech K485HW\r
-; Copyright Tripoli Motor Testing 1999 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-K485HW 54 699 0 0.910784 2.22029 AT\r
- 0.075 454.453\r
- 0.227 568.735\r
- 0.380 831.332\r
- 0.533 825.584\r
- 0.686 795.935\r
- 0.840 759.473\r
- 0.992 727.238\r
- 1.145 680.051\r
- 1.298 653.091\r
- 1.451 627.316\r
- 1.604 601.548\r
- 1.756 576.270\r
- 1.909 542.033\r
- 2.063 479.078\r
- 2.216 394.184\r
- 2.369 346.719\r
- 2.521 307.435\r
- 2.674 276.291\r
- 2.827 216.608\r
- 2.980 146.021\r
- 3.133 106.838\r
- 3.285 81.226\r
- 3.439 52.105\r
- 3.592 37.385\r
- 3.745 29.462\r
- 3.898 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="188.34" Itot="1682.18" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="431.549" burn-time="3.9" cgDiv="10" cgFix="1" cgStep="-1." code="K485HW" delays="1000" dia="54." exitDia="0." initWt="2220.29" len="699." mDiv="10" mFix="1" mStep="-1." massFrac="41.02" mfg="Aerotech" peakThrust="831.332" propWt="910.784" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AeroTech K485HW\r
+Copyright Tripoli Motor Testing 1999 (www.tripoli.org)\r
+provided by ThrustCurve.org (www.thrustcurve.org)\r
+</comments>\r
+<data>\r
+<eng-data cg="349.5" f="0." m="910.784" t="0."/>\r
+<eng-data cg="349.5" f="454.453" m="901.557" t="0.075"/>\r
+<eng-data cg="349.5" f="568.735" m="859.454" t="0.227"/>\r
+<eng-data cg="349.5" f="831.332" m="801.464" t="0.38"/>\r
+<eng-data cg="349.5" f="825.584" m="732.835" t="0.533"/>\r
+<eng-data cg="349.5" f="795.935" m="665.673" t="0.686"/>\r
+<eng-data cg="349.5" f="759.473" m="600.827" t="0.84"/>\r
+<eng-data cg="349.5" f="727.238" m="539.651" t="0.992"/>\r
+<eng-data cg="349.5" f="680.051" m="481.362" t="1.145"/>\r
+<eng-data cg="349.5" f="653.091" m="426.144" t="1.298"/>\r
+<eng-data cg="349.5" f="627.316" m="373.11" t="1.451"/>\r
+<eng-data cg="349.5" f="601.548" m="322.211" t="1.604"/>\r
+<eng-data cg="349.5" f="576.27" m="273.745" t="1.756"/>\r
+<eng-data cg="349.5" f="542.033" m="227.425" t="1.909"/>\r
+<eng-data cg="349.5" f="479.078" m="184.855" t="2.063"/>\r
+<eng-data cg="349.5" f="394.184" m="148.685" t="2.216"/>\r
+<eng-data cg="349.5" f="346.719" m="117.997" t="2.369"/>\r
+<eng-data cg="349.5" f="307.435" m="91.0794" t="2.521"/>\r
+<eng-data cg="349.5" f="276.291" m="66.9018" t="2.674"/>\r
+<eng-data cg="349.5" f="216.608" m="46.4861" t="2.827"/>\r
+<eng-data cg="349.5" f="146.021" m="31.4662" t="2.98"/>\r
+<eng-data cg="349.5" f="106.838" m="20.9929" t="3.133"/>\r
+<eng-data cg="349.5" f="81.226" m="13.2543" t="3.285"/>\r
+<eng-data cg="349.5" f="52.105" m="7.69571" t="3.439"/>\r
+<eng-data cg="349.5" f="37.385" m="3.98907" t="3.592"/>\r
+<eng-data cg="349.5" f="29.462" m="1.2203" t="3.745"/>\r
+<eng-data cg="349.5" f="0." m="0." t="3.898"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+; Input by Tim Van Milligan using ThrustCurve Tracer by John Coker. Data from\r
+; Tripoli certification paperwork dated 25 November 2007.\r
+K513FJ 54 410 6 0.974 1.647 Aerotech\r
+ 0.0070 555.093\r
+ 0.015 652.655\r
+ 0.041 551.729\r
+ 0.059 592.099\r
+ 0.074 551.729\r
+ 0.2 575.278\r
+ 0.282 582.007\r
+ 0.412 605.556\r
+ 0.519 615.649\r
+ 0.679 635.834\r
+ 0.823 642.562\r
+ 0.986 649.291\r
+ 1.12 652.655\r
+ 1.328 656.019\r
+ 1.48 649.291\r
+ 1.602 629.105\r
+ 1.854 585.371\r
+ 1.999 555.093\r
+ 2.054 545.0\r
+ 2.08 545.0\r
+ 2.114 528.179\r
+ 2.184 524.815\r
+ 2.229 521.451\r
+ 2.258 504.63\r
+ 2.295 474.352\r
+ 2.325 437.346\r
+ 2.358 380.155\r
+ 2.37 349.877\r
+ 2.399 312.871\r
+ 2.451 272.5\r
+ 2.492 238.858\r
+ 2.529 161.482\r
+ 2.57 84.105\r
+ 2.592 43.735\r
+ 2.618 26.914\r
+ 2.655 13.457\r
+ 2.692 6.728\r
+ 2.726 0.0\r
+++ /dev/null
-; AeroTech K550W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-K550W 54 410 0 0.919744 1.48736 AT\r
- 0.065 604.264\r
- 0.196 642.625\r
- 0.327 682.197\r
- 0.458 732.995\r
- 0.591 758.236\r
- 0.723 780.289\r
- 0.854 794.452\r
- 0.985 797.939\r
- 1.117 797.601\r
- 1.249 773.842\r
- 1.381 711.608\r
- 1.512 646.522\r
- 1.644 590.724\r
- 1.775 537.505\r
- 1.907 491.012\r
- 2.040 445.836\r
- 2.171 401.461\r
- 2.302 364.291\r
- 2.433 319.614\r
- 2.566 255.577\r
- 2.698 172.573\r
- 2.829 103.501\r
- 2.960 51.795\r
- 3.092 26.814\r
- 3.224 15.203\r
- 3.356 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="184.68" Itot="1594.46" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="455.561" burn-time="3.5" cgDiv="10" cgFix="1" cgStep="-1." code="K550W" delays="6,10,14,18" dia="54." exitDia="0." initWt="1515.1" len="410." mDiv="10" mFix="1" mStep="-1." massFrac="58.11" mfg="Aerotech" peakThrust="853.13" propWt="880.4" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="205." f="0." m="880.4" t="0."/>\r
+<eng-data cg="205." f="628.15" m="880.4" t="0."/>\r
+<eng-data cg="205." f="853.13" m="839.505" t="0.1"/>\r
+<eng-data cg="205." f="695.98" m="796.737" t="0.2"/>\r
+<eng-data cg="205." f="628.64" m="760.167" t="0.3"/>\r
+<eng-data cg="205." f="606.17" m="623.804" t="0.7"/>\r
+<eng-data cg="205." f="606.17" m="456.452" t="1.2"/>\r
+<eng-data cg="205." f="588.2" m="324.555" t="1.6"/>\r
+<eng-data cg="205." f="543.32" m="262.077" t="1.8"/>\r
+<eng-data cg="205." f="435.55" m="72.9046" t="2.5"/>\r
+<eng-data cg="205." f="89.85" m="14.8835" t="2.9"/>\r
+<eng-data cg="205." f="0." m="0." t="3.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech K560W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-K560W 75 396 0 1.40806 2.71354 AT\r
- 0.096 552.123\r
- 0.290 645.403\r
- 0.484 681.109\r
- 0.679 716.167\r
- 0.874 742.678\r
- 1.069 764.778\r
- 1.264 775.710\r
- 1.458 785.859\r
- 1.653 789.305\r
- 1.848 789.077\r
- 2.043 744.622\r
- 2.237 676.886\r
- 2.432 614.711\r
- 2.627 557.908\r
- 2.822 503.641\r
- 3.017 455.504\r
- 3.211 412.045\r
- 3.406 372.963\r
- 3.601 335.987\r
- 3.796 307.346\r
- 3.991 279.856\r
- 4.185 223.491\r
- 4.380 70.441\r
- 4.575 10.028\r
- 4.770 2.445\r
- 4.965 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="178.67" Itot="2467.2" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="496.918" burn-time="4.96" cgDiv="10" cgFix="1" cgStep="-1." code="K560W" delays="1000" dia="75." exitDia="0." initWt="2713.54" len="396." mDiv="10" mFix="1" mStep="-1." massFrac="51.89" mfg="Aerotech" peakThrust="789.305" propWt="1408.06" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="198." f="0." m="1408.06" t="0."/>\r
+<eng-data cg="198." f="552.123" m="1392.94" t="0.096"/>\r
+<eng-data cg="198." f="645.403" m="1326.64" t="0.29"/>\r
+<eng-data cg="198." f="681.109" m="1253.21" t="0.484"/>\r
+<eng-data cg="198." f="716.167" m="1175.46" t="0.679"/>\r
+<eng-data cg="198." f="742.678" m="1094.28" t="0.874"/>\r
+<eng-data cg="198." f="764.778" m="1010.4" t="1.069"/>\r
+<eng-data cg="198." f="775.71" m="924.678" t="1.264"/>\r
+<eng-data cg="198." f="785.859" m="838.231" t="1.458"/>\r
+<eng-data cg="198." f="789.305" m="750.582" t="1.653"/>\r
+<eng-data cg="198." f="789.077" m="662.754" t="1.848"/>\r
+<eng-data cg="198." f="744.622" m="577.412" t="2.043"/>\r
+<eng-data cg="198." f="676.886" m="498.718" t="2.237"/>\r
+<eng-data cg="198." f="614.711" m="426.848" t="2.432"/>\r
+<eng-data cg="198." f="557.908" m="361.598" t="2.627"/>\r
+<eng-data cg="198." f="503.641" m="302.529" t="2.822"/>\r
+<eng-data cg="198." f="455.504" m="249.158" t="3.017"/>\r
+<eng-data cg="198." f="412.045" m="201.131" t="3.211"/>\r
+<eng-data cg="198." f="372.963" m="157.45" t="3.406"/>\r
+<eng-data cg="198." f="335.987" m="118.001" t="3.601"/>\r
+<eng-data cg="198." f="307.346" m="82.2028" t="3.796"/>\r
+<eng-data cg="198." f="279.856" m="49.5283" t="3.991"/>\r
+<eng-data cg="198." f="223.491" m="21.6634" t="4.185"/>\r
+<eng-data cg="198." f="70.441" m="5.30776" t="4.38"/>\r
+<eng-data cg="198." f="10.028" m="0.830104" t="4.575"/>\r
+<eng-data cg="198." f="2.445" m="0.136051" t="4.77"/>\r
+<eng-data cg="198." f="0." m="0." t="4.965"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech K650T\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-K650T 98 289 0 1.27008 2.9353 AT\r
- 0.079 514.338\r
- 0.240 594.264\r
- 0.401 618.849\r
- 0.563 641.658\r
- 0.723 665.057\r
- 0.884 686.488\r
- 1.046 704.685\r
- 1.206 720.215\r
- 1.368 730.072\r
- 1.529 736.891\r
- 1.690 743.109\r
- 1.851 747.503\r
- 2.013 747.557\r
- 2.174 744.081\r
- 2.335 732.294\r
- 2.496 710.412\r
- 2.657 682.670\r
- 2.819 653.246\r
- 2.979 627.020\r
- 3.141 595.456\r
- 3.302 563.844\r
- 3.463 551.080\r
- 3.624 236.059\r
- 3.785 1.383\r
- 3.947 1.234\r
- 4.108 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="191.71" Itot="2387.85" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="581.268" burn-time="4.11" cgDiv="10" cgFix="1" cgStep="-1." code="K650T" delays="1000" dia="98." exitDia="0." initWt="2935.3" len="289." mDiv="10" mFix="1" mStep="-1." massFrac="43.27" mfg="Aerotech" peakThrust="747.557" propWt="1270.08" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AeroTech K650T\r
+Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
+provided by ThrustCurve.org (www.thrustcurve.org)\r
+</comments>\r
+<data>\r
+<eng-data cg="144.5" f="0." m="1270.08" t="0."/>\r
+<eng-data cg="144.5" f="514.338" m="1259.27" t="0.079"/>\r
+<eng-data cg="144.5" f="594.264" m="1211.81" t="0.24"/>\r
+<eng-data cg="144.5" f="618.849" m="1159.86" t="0.401"/>\r
+<eng-data cg="144.5" f="641.658" m="1105.56" t="0.563"/>\r
+<eng-data cg="144.5" f="665.057" m="1049.95" t="0.723"/>\r
+<eng-data cg="144.5" f="686.488" m="992.085" t="0.884"/>\r
+<eng-data cg="144.5" f="704.685" m="932.149" t="1.046"/>\r
+<eng-data cg="144.5" f="720.215" m="871.517" t="1.206"/>\r
+<eng-data cg="144.5" f="730.072" m="809.034" t="1.368"/>\r
+<eng-data cg="144.5" f="736.891" m="746.222" t="1.529"/>\r
+<eng-data cg="144.5" f="743.109" m="682.853" t="1.69"/>\r
+<eng-data cg="144.5" f="747.503" m="619.029" t="1.851"/>\r
+<eng-data cg="144.5" f="747.557" m="554.617" t="2.013"/>\r
+<eng-data cg="144.5" f="744.081" m="490.748" t="2.174"/>\r
+<eng-data cg="144.5" f="732.294" m="427.534" t="2.335"/>\r
+<eng-data cg="144.5" f="710.412" m="365.761" t="2.496"/>\r
+<eng-data cg="144.5" f="682.67" m="306.113" t="2.657"/>\r
+<eng-data cg="144.5" f="653.246" m="248.557" t="2.819"/>\r
+<eng-data cg="144.5" f="627.02" m="194.08" t="2.979"/>\r
+<eng-data cg="144.5" f="595.456" m="141.412" t="3.141"/>\r
+<eng-data cg="144.5" f="563.844" m="91.7736" t="3.302"/>\r
+<eng-data cg="144.5" f="551.08" m="44.0355" t="3.463"/>\r
+<eng-data cg="144.5" f="236.059" m="10.3322" t="3.624"/>\r
+<eng-data cg="144.5" f="1.383" m="0.165586" t="3.785"/>\r
+<eng-data cg="144.5" f="1.234" m="0.0528366" t="3.947"/>\r
+<eng-data cg="144.5" f="0." m="0." t="4.108"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech K680R RASP engine file\r
-;Data Entered by Tim Van Milligan\r
-;Source: TRA Certification paperwork, and\r
-;Aerotech's instruction sheet: RMS 98/2560-10240 REDLINE.\r
-K680R 98 289 100 1.316 3.035 AT\r
-0.085 629.798\r
-0.494 717.881\r
-0.996 797.157\r
-1.29 819.178\r
-1.506 819.178\r
-2.001 775.136\r
-2.519 673.84\r
-2.99 563.735\r
-3.137 541.714\r
-3.176 532.906\r
-3.238 563.735\r
-3.276 563.735\r
-3.408 52.85\r
-3.431 22.02\r
-3.49 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="182.74" Itot="2358.34" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="675.742" burn-time="3.49" cgDiv="10" cgFix="1" cgStep="-1." code="K680R" delays="1000" dia="98." exitDia="0." initWt="3035." len="289." mDiv="10" mFix="1" mStep="-1." massFrac="43.36" mfg="Aerotech" peakThrust="819.178" propWt="1316." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech K680R RASP engine file\r
+Data Entered by Tim Van Milligan\r
+Source: TRA Certification paperwork, and\r
+Aerotech's instruction sheet: RMS 98/2560-10240 REDLINE.\r
+</comments>\r
+<data>\r
+<eng-data cg="144.5" f="0." m="1316." t="0."/>\r
+<eng-data cg="144.5" f="629.798" m="1301.06" t="0.085"/>\r
+<eng-data cg="144.5" f="717.881" m="1147.27" t="0.494"/>\r
+<eng-data cg="144.5" f="797.157" m="935.073" t="0.996"/>\r
+<eng-data cg="144.5" f="819.178" m="802.487" t="1.29"/>\r
+<eng-data cg="144.5" f="819.178" m="703.749" t="1.506"/>\r
+<eng-data cg="144.5" f="775.136" m="483.559" t="2.001"/>\r
+<eng-data cg="144.5" f="673.84" m="274.142" t="2.519"/>\r
+<eng-data cg="144.5" f="563.735" m="111.508" t="2.99"/>\r
+<eng-data cg="144.5" f="541.714" m="66.1689" t="3.137"/>\r
+<eng-data cg="144.5" f="532.906" m="54.4756" t="3.176"/>\r
+<eng-data cg="144.5" f="563.735" m="35.5052" t="3.238"/>\r
+<eng-data cg="144.5" f="563.735" m="23.5513" t="3.276"/>\r
+<eng-data cg="144.5" f="52.85" m="0.842942" t="3.408"/>\r
+<eng-data cg="144.5" f="22.02" m="0.362484" t="3.431"/>\r
+<eng-data cg="144.5" f="0." m="0." t="3.49"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech K695R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-K695R 54 410 0 0.9184 1.48736 AT\r
- 0.044 618.611\r
- 0.134 727.840\r
- 0.224 751.996\r
- 0.314 812.480\r
- 0.404 900.125\r
- 0.495 884.763\r
- 0.585 873.457\r
- 0.675 864.561\r
- 0.765 849.672\r
- 0.856 838.886\r
- 0.946 822.550\r
- 1.036 806.240\r
- 1.126 781.342\r
- 1.216 753.973\r
- 1.307 728.472\r
- 1.398 697.629\r
- 1.487 672.979\r
- 1.578 646.660\r
- 1.667 620.897\r
- 1.758 595.574\r
- 1.849 571.720\r
- 1.939 546.822\r
- 2.029 272.824\r
- 2.119 57.950\r
- 2.209 4.509\r
- 2.300 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="163.91" Itot="1496.47" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="665.099" burn-time="2.25" cgDiv="10" cgFix="1" cgStep="-1." code="K695R" delays="10,14,1000" dia="54." exitDia="0." initWt="1506." len="410." mDiv="10" mFix="1" mStep="-1." massFrac="61.82" mfg="Aerotech" peakThrust="900.13" propWt="931." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="205." f="0." m="931." t="0."/>\r
+<eng-data cg="205." f="618.61" m="923.303" t="0.04"/>\r
+<eng-data cg="205." f="727.84" m="885.608" t="0.13"/>\r
+<eng-data cg="205." f="752." m="844.179" t="0.22"/>\r
+<eng-data cg="205." f="812.48" m="800.38" t="0.31"/>\r
+<eng-data cg="205." f="900.13" m="752.434" t="0.4"/>\r
+<eng-data cg="205." f="884.76" m="696.912" t="0.5"/>\r
+<eng-data cg="205." f="873.46" m="653.158" t="0.58"/>\r
+<eng-data cg="205." f="864.56" m="599.095" t="0.68"/>\r
+<eng-data cg="205." f="849.67" m="551.104" t="0.77"/>\r
+<eng-data cg="205." f="838.89" m="503.831" t="0.86"/>\r
+<eng-data cg="205." f="822.55" m="457.318" t="0.95"/>\r
+<eng-data cg="205." f="806.24" m="411.718" t="1.04"/>\r
+<eng-data cg="205." f="781.34" m="367.273" t="1.13"/>\r
+<eng-data cg="205." f="753.97" m="324.29" t="1.22"/>\r
+<eng-data cg="205." f="728.47" m="282.788" t="1.31"/>\r
+<eng-data cg="205." f="697.63" m="242.863" t="1.4"/>\r
+<eng-data cg="205." f="672.98" m="204.492" t="1.49"/>\r
+<eng-data cg="205." f="646.66" m="167.548" t="1.58"/>\r
+<eng-data cg="205." f="620.9" m="132.061" t="1.67"/>\r
+<eng-data cg="205." f="595.57" m="98.0051" t="1.76"/>\r
+<eng-data cg="205." f="571.72" m="65.3259" t="1.85"/>\r
+<eng-data cg="205." f="546.82" m="34.0114" t="1.94"/>\r
+<eng-data cg="205." f="272.82" m="11.0649" t="2.03"/>\r
+<eng-data cg="205." f="57.95" m="1.80474" t="2.12"/>\r
+<eng-data cg="205." f="4.51" m="0.0561161" t="2.21"/>\r
+<eng-data cg="205." f="0." m="0." t="2.25"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech K700W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-K700W 54 568 0 1.29158 2.03526 AT\r
- 0.069 1005.472\r
- 0.209 1018.916\r
- 0.350 1026.610\r
- 0.491 1028.637\r
- 0.632 1029.337\r
- 0.773 1004.203\r
- 0.914 970.694\r
- 1.055 946.516\r
- 1.196 918.437\r
- 1.336 873.783\r
- 1.478 821.276\r
- 1.619 773.270\r
- 1.759 735.553\r
- 1.900 692.732\r
- 2.041 658.984\r
- 2.182 626.737\r
- 2.323 591.431\r
- 2.464 508.666\r
- 2.605 420.175\r
- 2.746 328.309\r
- 2.886 202.409\r
- 3.028 121.672\r
- 3.169 80.453\r
- 3.309 50.873\r
- 3.451 31.548\r
- 3.593 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="180.3" Itot="2283.68" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="635.592" burn-time="3.59" cgDiv="10" cgFix="1" cgStep="-1." code="K700W" delays="1000" dia="54." exitDia="0." initWt="2035.26" len="568." mDiv="10" mFix="1" mStep="-1." massFrac="63.46" mfg="Aerotech" peakThrust="1029.34" propWt="1291.58" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AeroTech K700W\r
+Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
+provided by ThrustCurve.org (www.thrustcurve.org)\r
+</comments>\r
+<data>\r
+<eng-data cg="284." f="0." m="1291.58" t="0."/>\r
+<eng-data cg="284." f="1005.47" m="1271.96" t="0.069"/>\r
+<eng-data cg="284." f="1018.92" m="1191.82" t="0.209"/>\r
+<eng-data cg="284." f="1026.61" m="1110.26" t="0.35"/>\r
+<eng-data cg="284." f="1028.64" m="1028.31" t="0.491"/>\r
+<eng-data cg="284." f="1029.34" m="946.25" t="0.632"/>\r
+<eng-data cg="284." f="1004.2" m="865.167" t="0.773"/>\r
+<eng-data cg="284." f="970.694" m="786.423" t="0.914"/>\r
+<eng-data cg="284." f="946.516" m="709.979" t="1.055"/>\r
+<eng-data cg="284." f="918.437" m="635.618" t="1.196"/>\r
+<eng-data cg="284." f="873.783" m="564.664" t="1.336"/>\r
+<eng-data cg="284." f="821.276" m="496.598" t="1.478"/>\r
+<eng-data cg="284." f="773.27" m="433.02" t="1.619"/>\r
+<eng-data cg="284." f="735.553" m="373.285" t="1.759"/>\r
+<eng-data cg="284." f="692.732" m="316.336" t="1.9"/>\r
+<eng-data cg="284." f="658.984" m="262.439" t="2.041"/>\r
+<eng-data cg="284." f="626.737" m="211.174" t="2.182"/>\r
+<eng-data cg="284." f="591.431" m="162.603" t="2.323"/>\r
+<eng-data cg="284." f="508.666" m="118.739" t="2.464"/>\r
+<eng-data cg="284." f="420.175" m="81.7036" t="2.605"/>\r
+<eng-data cg="284." f="328.309" m="51.8596" t="2.746"/>\r
+<eng-data cg="284." f="202.409" m="30.8485" t="2.886"/>\r
+<eng-data cg="284." f="121.672" m="17.8349" t="3.028"/>\r
+<eng-data cg="284." f="80.453" m="9.77565" t="3.169"/>\r
+<eng-data cg="284." f="50.873" m="4.57647" t="3.309"/>\r
+<eng-data cg="284." f="31.548" m="1.26682" t="3.451"/>\r
+<eng-data cg="284." f="0." m="0." t="3.593"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech K780R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-K780R 75 289 0 1.26784 2.9344 AT\r
- 0.053 383.290\r
- 0.173 718.241\r
- 0.292 849.343\r
- 0.413 885.503\r
- 0.533 903.243\r
- 0.652 924.403\r
- 0.772 938.825\r
- 0.892 938.623\r
- 1.013 947.130\r
- 1.133 953.578\r
- 1.253 944.001\r
- 1.373 935.448\r
- 1.495 929.447\r
- 1.617 920.379\r
- 1.737 897.293\r
- 1.857 888.917\r
- 1.977 861.127\r
- 2.098 840.971\r
- 2.217 812.360\r
- 2.337 779.614\r
- 2.457 747.866\r
- 2.578 726.819\r
- 2.697 729.258\r
- 2.817 279.891\r
- 2.940 10.969\r
- 3.063 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="189.9" Itot="2361.06" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="770.832" burn-time="3.06" cgDiv="10" cgFix="1" cgStep="-1." code="K780R" delays="1000" dia="75." exitDia="0." initWt="2934.4" len="395." mDiv="10" mFix="1" mStep="-1." massFrac="43.21" mfg="Aerotech" peakThrust="953.578" propWt="1267.84" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AeroTech K780R\r
+provided by ThrustCurve.org (www.thrustcurve.org)\r
+</comments>\r
+<data>\r
+<eng-data cg="197.5" f="0." m="1267.84" t="0."/>\r
+<eng-data cg="197.5" f="383.29" m="1262.39" t="0.053"/>\r
+<eng-data cg="197.5" f="718.241" m="1226.9" t="0.173"/>\r
+<eng-data cg="197.5" f="849.343" m="1176.81" t="0.292"/>\r
+<eng-data cg="197.5" f="885.503" m="1120.45" t="0.413"/>\r
+<eng-data cg="197.5" f="903.243" m="1062.82" t="0.533"/>\r
+<eng-data cg="197.5" f="924.403" m="1004.43" t="0.652"/>\r
+<eng-data cg="197.5" f="938.825" m="944.395" t="0.772"/>\r
+<eng-data cg="197.5" f="938.623" m="883.906" t="0.892"/>\r
+<eng-data cg="197.5" f="947.13" m="822.643" t="1.013"/>\r
+<eng-data cg="197.5" f="953.578" m="761.404" t="1.133"/>\r
+<eng-data cg="197.5" f="944.001" m="700.267" t="1.253"/>\r
+<eng-data cg="197.5" f="935.448" m="639.713" t="1.373"/>\r
+<eng-data cg="197.5" f="929.447" m="578.627" t="1.495"/>\r
+<eng-data cg="197.5" f="920.379" m="518.035" t="1.617"/>\r
+<eng-data cg="197.5" f="897.293" m="459.471" t="1.737"/>\r
+<eng-data cg="197.5" f="888.917" m="401.922" t="1.857"/>\r
+<eng-data cg="197.5" f="861.127" m="345.538" t="1.977"/>\r
+<eng-data cg="197.5" f="840.971" m="290.241" t="2.098"/>\r
+<eng-data cg="197.5" f="812.36" m="237.417" t="2.217"/>\r
+<eng-data cg="197.5" f="779.614" m="186.125" t="2.337"/>\r
+<eng-data cg="197.5" f="747.866" m="136.912" t="2.457"/>\r
+<eng-data cg="197.5" f="726.819" m="89.0033" t="2.578"/>\r
+<eng-data cg="197.5" f="729.258" m="42.4812" t="2.697"/>\r
+<eng-data cg="197.5" f="279.891" m="9.96767" t="2.817"/>\r
+<eng-data cg="197.5" f="10.969" m="0.362243" t="2.94"/>\r
+<eng-data cg="197.5" f="0." m="0." t="3.063"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+; From the curve of the motor instruction sheet.\r
+; Made using Thrust Curve Tracer.\r
+; Tom Koszuta 12/26/2008.\r
+K805G 54 410 P 0.871 1.543 AT\r
+ 0.0050 443.21\r
+ 0.032 817.925\r
+ 0.053 825.983\r
+ 0.098 854.187\r
+ 0.199 902.537\r
+ 0.298 918.654\r
+ 0.399 938.8\r
+ 0.5 950.888\r
+ 0.595 950.888\r
+ 0.699 950.888\r
+ 0.8 942.829\r
+ 0.903 934.771\r
+ 1.002 922.683\r
+ 1.1 902.537\r
+ 1.201 874.333\r
+ 1.254 866.275\r
+ 1.267 878.362\r
+ 1.299 854.187\r
+ 1.334 846.129\r
+ 1.35 850.158\r
+ 1.398 821.954\r
+ 1.499 781.662\r
+ 1.522 789.72\r
+ 1.536 781.662\r
+ 1.546 765.545\r
+ 1.597 757.487\r
+ 1.698 721.224\r
+ 1.799 701.078\r
+ 1.897 688.991\r
+ 1.95 693.02\r
+ 1.961 705.107\r
+ 1.982 697.049\r
+ 1.995 668.845\r
+ 2.014 596.319\r
+ 2.035 447.24\r
+ 2.051 342.481\r
+ 2.064 269.955\r
+ 2.08 205.488\r
+ 2.099 165.197\r
+ 2.123 120.876\r
+ 2.147 84.613\r
+ 2.171 52.379\r
+ 2.197 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="AT" code="K715G-P" Type="reloadable" dia="54." len="400.6" initWt="1543."\r
+propWt="871.1" auto-calc-mass="1" auto-calc-cg="1" avgThrust="720.852"\r
+peakThrust="828.29" throatDia="0." exitDia="0." Itot="1730.04" burn-time="2.4"\r
+massFrac="56.45" Isp="202.52" tDiv="25" tStep="-0.1" tFix="1" FDiv="20"\r
+FStep="-10." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."\r
+cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="871.1" cg="853."/>\r
+ <eng-data t="0." f="7.66935" m="871.1" cg="853."/>\r
+ <eng-data t="0.00388199" f="437.153" m="870.665" cg="853."/>\r
+ <eng-data t="0.0427019" f="797.612" m="858.598" cg="853."/>\r
+ <eng-data t="0.0776398" f="828.29" m="844.296" cg="853."/>\r
+ <eng-data t="0.100932" f="774.604" m="834.897" cg="853."/>\r
+ <eng-data t="0.159161" f="736.257" m="812.748" cg="853."/>\r
+ <eng-data t="0.197981" f="743.927" m="798.282" cg="853."/>\r
+ <eng-data t="0.298913" f="774.604" m="759.696" cg="853."/>\r
+ <eng-data t="0.399845" f="789.943" m="719.94" cg="853."/>\r
+ <eng-data t="0.500776" f="797.612" m="679.6" cg="853."/>\r
+ <eng-data t="0.601708" f="812.951" m="638.675" cg="853."/>\r
+ <eng-data t="0.698758" f="812.951" m="598.95" cg="853."/>\r
+ <eng-data t="0.799689" f="812.951" m="557.635" cg="853."/>\r
+ <eng-data t="0.900621" f="812.951" m="516.321" cg="853."/>\r
+ <eng-data t="1.00155" f="812.951" m="475.006" cg="853."/>\r
+ <eng-data t="1.0986" f="782.274" m="436.03" cg="853."/>\r
+ <eng-data t="1.19953" f="766.935" m="396.664" cg="853."/>\r
+ <eng-data t="1.29658" f="759.265" m="359.374" cg="853."/>\r
+ <eng-data t="1.4014" f="759.265" m="319.304" cg="853."/>\r
+ <eng-data t="1.49845" f="743.927" m="282.577" cg="853."/>\r
+ <eng-data t="1.59938" f="720.919" m="245.355" cg="853."/>\r
+ <eng-data t="1.69643" f="697.911" m="210.688" cg="853."/>\r
+ <eng-data t="1.80124" f="682.572" m="174.261" cg="853."/>\r
+ <eng-data t="1.89829" f="659.564" m="141.468" cg="853."/>\r
+ <eng-data t="1.99922" f="644.225" m="108.339" cg="853."/>\r
+ <eng-data t="2.10016" f="628.887" m="75.9886" cg="853."/>\r
+ <eng-data t="2.20109" f="644.225" m="43.6385" cg="853."/>\r
+ <eng-data t="2.30202" f="544.524" m="13.432" cg="853."/>\r
+ <eng-data t="2.4" f="0." m="0." cg="853."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-K828FJ 54.0 579.00 6-10-14-18 1.45000 2.25500 AT\r
- 0.01 1112.06 \r
- 0.02 1238.60 \r
- 0.04 1303.79 \r
- 0.06 1135.06 \r
- 0.08 1077.54 \r
- 0.13 1031.53 \r
- 0.20 1016.19 \r
- 0.50 993.18 \r
- 0.65 1004.68 \r
- 1.00 985.51 \r
- 1.08 974.01 \r
- 1.19 974.01 \r
- 1.42 954.83 \r
- 1.51 935.66 \r
- 1.69 912.65 \r
- 1.75 885.81 \r
- 1.83 893.48 \r
- 1.89 843.63 \r
- 1.95 774.60 \r
- 2.00 667.23 \r
- 2.15 444.82 \r
- 2.20 364.29 \r
- 2.23 260.76 \r
- 2.27 184.06 \r
- 2.33 111.21 \r
- 2.39 49.85 \r
- 2.50 0.00 \r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="AT-RMS" code="K828FJ" Type="reloadable" dia="54." len="579." initWt="2223."\r
+propWt="1373." auto-calc-mass="1" auto-calc-cg="1" avgThrust="862.878"\r
+peakThrust="1303.79" throatDia="0." exitDia="0." Itot="2157.2" burn-time="2.5"\r
+massFrac="61.76" Isp="160.21" tDiv="10" tStep="-1." tFix="1" FDiv="10"\r
+FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."\r
+cgFix="1">\r
+ <comments>Cert data from TRA\r
+Converted from Mark Koelsch</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="1373." cg="289.5"/>\r
+ <eng-data t="0.01" f="1112.06" m="1369.46" cg="289.5"/>\r
+ <eng-data t="0.02" f="1112.06" m="1362.38" cg="289.5"/>\r
+ <eng-data t="0.04" f="1238.6" m="1347.42" cg="289.5"/>\r
+ <eng-data t="0.06" f="1303.79" m="1331.24" cg="289.5"/>\r
+ <eng-data t="0.08" f="1135.06" m="1315.72" cg="289.5"/>\r
+ <eng-data t="0.13" f="1077.54" m="1280.51" cg="289.5"/>\r
+ <eng-data t="0.2" f="1031.53" m="1233.53" cg="289.5"/>\r
+ <eng-data t="0.5" f="1016.19" m="1038.03" cg="289.5"/>\r
+ <eng-data t="0.65" f="993.18" m="942.111" cg="289.5"/>\r
+ <eng-data t="1." f="1004.68" m="719.583" cg="289.5"/>\r
+ <eng-data t="1.08" f="985.51" m="668.915" cg="289.5"/>\r
+ <eng-data t="1.19" f="974.01" m="600.32" cg="289.5"/>\r
+ <eng-data t="1.42" f="974.01" m="457.735" cg="289.5"/>\r
+ <eng-data t="1.51" f="954.83" m="402.491" cg="289.5"/>\r
+ <eng-data t="1.69" f="935.66" m="294.198" cg="289.5"/>\r
+ <eng-data t="1.75" f="912.65" m="258.906" cg="289.5"/>\r
+ <eng-data t="1.83" f="885.81" m="213.119" cg="289.5"/>\r
+ <eng-data t="1.89" f="893.48" m="179.145" cg="289.5"/>\r
+ <eng-data t="1.95" f="843.63" m="145.976" cg="289.5"/>\r
+ <eng-data t="2." f="774.6" m="120.227" cg="289.5"/>\r
+ <eng-data t="2.15" f="667.23" m="51.4005" cg="289.5"/>\r
+ <eng-data t="2.2" f="444.82" m="33.7057" cg="289.5"/>\r
+ <eng-data t="2.23" f="364.29" m="25.9811" cg="289.5"/>\r
+ <eng-data t="2.27" f="260.76" m="18.0245" cg="289.5"/>\r
+ <eng-data t="2.33" f="184.06" m="9.53099" cg="289.5"/>\r
+ <eng-data t="2.39" f="111.21" m="3.89303" cg="289.5"/>\r
+ <eng-data t="2.5" f="0." m="0." cg="289.5"/>\r
+ <eng-data t="2.5" f="49.85" m="0." cg="289.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech L1120W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-L1120W 75 665 0 2.75699 4.65786 AT\r
- 0.097 1377.215\r
- 0.293 1442.670\r
- 0.489 1496.986\r
- 0.685 1537.057\r
- 0.882 1554.962\r
- 1.078 1554.131\r
- 1.275 1547.973\r
- 1.472 1533.465\r
- 1.668 1510.342\r
- 1.865 1472.279\r
- 2.061 1362.534\r
- 2.257 1245.425\r
- 2.454 1148.864\r
- 2.651 1062.680\r
- 2.847 984.952\r
- 3.044 916.169\r
- 3.241 831.929\r
- 3.436 766.450\r
- 3.633 698.978\r
- 3.830 562.966\r
- 4.026 384.579\r
- 4.223 227.654\r
- 4.420 105.078\r
- 4.616 56.339\r
- 4.813 21.712\r
- 5.009 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="182.06" Itot="4922.22" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="982.675" burn-time="5.01" cgDiv="10" cgFix="1" cgStep="-1." code="L1120W" delays="1000" dia="75." exitDia="0." initWt="4657.86" len="665." mDiv="10" mFix="1" mStep="-1." massFrac="59.19" mfg="Aerotech" peakThrust="1554.96" propWt="2756.99" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="332.5" f="0." m="2756.99" t="0."/>\r
+<eng-data cg="332.5" f="1377.21" m="2719.58" t="0.097"/>\r
+<eng-data cg="332.5" f="1442.67" m="2564.79" t="0.293"/>\r
+<eng-data cg="332.5" f="1496.99" m="2403.43" t="0.489"/>\r
+<eng-data cg="332.5" f="1537.06" m="2236.89" t="0.685"/>\r
+<eng-data cg="332.5" f="1554.96" m="2066.3" t="0.882"/>\r
+<eng-data cg="332.5" f="1554.13" m="1895.64" t="1.078"/>\r
+<eng-data cg="332.5" f="1547.97" m="1724.49" t="1.275"/>\r
+<eng-data cg="332.5" f="1533.46" m="1554.49" t="1.472"/>\r
+<eng-data cg="332.5" f="1510.34" m="1387.41" t="1.668"/>\r
+<eng-data cg="332.5" f="1472.28" m="1222.86" t="1.865"/>\r
+<eng-data cg="332.5" f="1362.53" m="1067.25" t="2.061"/>\r
+<eng-data cg="332.5" f="1245.42" m="924.099" t="2.257"/>\r
+<eng-data cg="332.5" f="1148.86" m="792.005" t="2.454"/>\r
+<eng-data cg="332.5" f="1062.68" m="669.992" t="2.651"/>\r
+<eng-data cg="332.5" f="984.952" m="557.596" t="2.847"/>\r
+<eng-data cg="332.5" f="916.169" m="452.709" t="3.044"/>\r
+<eng-data cg="332.5" f="831.929" m="356.265" t="3.241"/>\r
+<eng-data cg="332.5" f="766.45" m="268.976" t="3.436"/>\r
+<eng-data cg="332.5" f="698.978" m="188.127" t="3.633"/>\r
+<eng-data cg="332.5" f="562.966" m="118.504" t="3.83"/>\r
+<eng-data cg="332.5" f="384.579" m="66.4929" t="4.026"/>\r
+<eng-data cg="332.5" f="227.654" m="32.7154" t="4.223"/>\r
+<eng-data cg="332.5" f="105.078" m="14.3583" t="4.42"/>\r
+<eng-data cg="332.5" f="56.339" m="5.49794" t="4.616"/>\r
+<eng-data cg="332.5" f="21.712" m="1.19179" t="4.813"/>\r
+<eng-data cg="332.5" f="0." m="0." t="5.009"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech L1150\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-L1150 75 531 0 2.06528 3.6736 AT\r
- 0.053 935.855\r
- 0.175 1292.642\r
- 0.300 1260.926\r
- 0.425 1241.482\r
- 0.550 1257.058\r
- 0.675 1272.287\r
- 0.800 1287.605\r
- 0.925 1301.012\r
- 1.048 1309.708\r
- 1.170 1308.417\r
- 1.295 1304.830\r
- 1.420 1285.265\r
- 1.545 1267.657\r
- 1.670 1255.624\r
- 1.795 1227.212\r
- 1.920 1202.443\r
- 2.043 1182.617\r
- 2.165 1150.712\r
- 2.290 1117.909\r
- 2.415 1081.739\r
- 2.540 1037.547\r
- 2.665 1007.091\r
- 2.790 1008.911\r
- 2.915 643.124\r
- 3.040 64.371\r
- 3.165 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="172.24" Itot="3488.55" Type="unspecified" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1102.23" burn-time="3.17" cgDiv="10" cgFix="1" cgStep="-1." code="L1150" delays="1000" dia="75." exitDia="0." initWt="3673.6" len="531." mDiv="10" mFix="1" mStep="-1." massFrac="56.22" mfg="Aerotech" peakThrust="1309.71" propWt="2065.28" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AeroTech L1150\r
+provided by ThrustCurve.org (www.thrustcurve.org)\r
+</comments>\r
+<data>\r
+<eng-data cg="265.5" f="0." m="2065.28" t="0."/>\r
+<eng-data cg="265.5" f="935.855" m="2050.6" t="0.053"/>\r
+<eng-data cg="265.5" f="1292.64" m="1970.12" t="0.175"/>\r
+<eng-data cg="265.5" f="1260.93" m="1875.64" t="0.3"/>\r
+<eng-data cg="265.5" f="1241.48" m="1783.04" t="0.425"/>\r
+<eng-data cg="265.5" f="1257.06" m="1690.6" t="0.55"/>\r
+<eng-data cg="265.5" f="1272.29" m="1597.01" t="0.675"/>\r
+<eng-data cg="265.5" f="1287.61" m="1502.29" t="0.8"/>\r
+<eng-data cg="265.5" f="1301.01" m="1406.51" t="0.925"/>\r
+<eng-data cg="265.5" f="1309.71" m="1311.45" t="1.048"/>\r
+<eng-data cg="265.5" f="1308.42" m="1216.9" t="1.17"/>\r
+<eng-data cg="265.5" f="1304.83" m="1120.21" t="1.295"/>\r
+<eng-data cg="265.5" f="1285.27" m="1024.37" t="1.42"/>\r
+<eng-data cg="265.5" f="1267.66" m="929.913" t="1.545"/>\r
+<eng-data cg="265.5" f="1255.62" m="836.549" t="1.67"/>\r
+<eng-data cg="265.5" f="1227.21" m="744.682" t="1.795"/>\r
+<eng-data cg="265.5" f="1202.44" m="654.783" t="1.92"/>\r
+<eng-data cg="265.5" f="1182.62" m="567.945" t="2.043"/>\r
+<eng-data cg="265.5" f="1150.71" m="483.681" t="2.165"/>\r
+<eng-data cg="265.5" f="1117.91" m="399.74" t="2.29"/>\r
+<eng-data cg="265.5" f="1081.74" m="318.351" t="2.415"/>\r
+<eng-data cg="265.5" f="1037.55" m="239.935" t="2.54"/>\r
+<eng-data cg="265.5" f="1007.09" m="164.281" t="2.665"/>\r
+<eng-data cg="265.5" f="1008.91" m="89.6868" t="2.79"/>\r
+<eng-data cg="265.5" f="643.124" m="28.5598" t="2.915"/>\r
+<eng-data cg="265.5" f="64.371" m="2.38179" t="3.04"/>\r
+<eng-data cg="265.5" f="0." m="0." t="3.165"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+L1170FJ 75 665 P 2.8000000000000003 4.99 AT\r
+ 0.031 992.64\r
+ 0.072 1400.144\r
+ 0.113 1473.286\r
+ 0.144 1389.696\r
+ 0.351 1285.207\r
+ 1.495 1431.491\r
+ 1.856 1431.491\r
+ 2.227 1358.349\r
+ 2.753 1201.616\r
+ 2.928 1170.27\r
+ 3.0 1065.782\r
+ 3.113 679.175\r
+ 3.247 355.261\r
+ 3.361 177.63\r
+ 3.464 83.591\r
+ 3.67 0.0\r
+++ /dev/null
-;\r
-;\r
-L1300R 98 443 100 2.508 4.884 AT\r
-0.0231839 1299.23\r
-0.502318 1332.26\r
-0.996909 1497.42\r
-1.49923 1552.47\r
-1.99382 1508.43\r
-2.49614 1354.29\r
-2.99845 1101.05\r
-3.12983 1090.03\r
-3.21484 1145.09\r
-3.3694 176.167\r
-3.5 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="185.26" Itot="4556.42" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1301.84" burn-time="3.5" cgDiv="10" cgFix="1" cgStep="-1." code="L1300R" delays="1000" dia="98." exitDia="0." initWt="4884." len="443." mDiv="10" mFix="1" mStep="-1." massFrac="51.35" mfg="Aerotech" peakThrust="1552.47" propWt="2508." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="221.5" f="0." m="2508." t="0."/>\r
+<eng-data cg="221.5" f="1299.23" m="2499.71" t="0.0231839"/>\r
+<eng-data cg="221.5" f="1332.26" m="2152.71" t="0.502318"/>\r
+<eng-data cg="221.5" f="1497.42" m="1767.53" t="0.996909"/>\r
+<eng-data cg="221.5" f="1552.47" m="1345.9" t="1.49923"/>\r
+<eng-data cg="221.5" f="1508.43" m="929.249" t="1.99382"/>\r
+<eng-data cg="221.5" f="1354.29" m="533.488" t="2.49614"/>\r
+<eng-data cg="221.5" f="1101.05" m="194.053" t="2.99845"/>\r
+<eng-data cg="221.5" f="1090.03" m="114.828" t="3.12983"/>\r
+<eng-data cg="221.5" f="1145.09" m="62.5348" t="3.21484"/>\r
+<eng-data cg="221.5" f="176.167" m="6.33201" t="3.3694"/>\r
+<eng-data cg="221.5" f="0." m="0." t="3.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+;Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+;Tracer program. Thrust curve and engine data from Aerotech thrust stand.\r
+L1390G 75 517.91 1000 1.973 3.876 Aerotech \r
+0.018 906.203\r
+0.041 1249.41\r
+0.055 1336.72\r
+0.099 1369.84\r
+0.173 1402.96\r
+0.236 1411.99\r
+0.284 1411.99\r
+0.678 1586.61\r
+0.869 1649.83\r
+0.939 1640.8\r
+1.102 1625.74\r
+1.197 1628.76\r
+1.293 1619.72\r
+1.374 1607.68\r
+1.455 1601.66\r
+1.518 1589.62\r
+1.592 1550.48\r
+1.691 1499.3\r
+1.838 1424.03\r
+1.96 1366.83\r
+2.1 1312.64\r
+2.225 1261.46\r
+2.343 1228.34\r
+2.417 1213.29\r
+2.479 1204.26\r
+2.524 1198.23\r
+2.564 1198.23\r
+2.601 1165.12\r
+2.638 1074.8\r
+2.66 957.383\r
+2.689 839.968\r
+2.712 713.522\r
+2.737 590.085\r
+2.763 427.511\r
+2.8 295.043\r
+2.844 153.543\r
+2.877 69.245\r
+2.911 0\r
+++ /dev/null
-;\r
-;\r
-L1420R 75 443 100 2.56 4.562 AT\r
-0.0386399 1332.26\r
-0.123648 1563.48\r
-0.502318 1519.44\r
-0.996909 1574.49\r
-1.49923 1662.58\r
-2.00155 1574.49\r
-2.48068 1409.34\r
-2.92117 1299.23\r
-2.99073 1167.11\r
-3.11437 187.178\r
-3.24 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="183.88" Itot="4616.31" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1424.79" burn-time="3.24" cgDiv="10" cgFix="1" cgStep="-1." code="L1420R" delays="1000" dia="75." exitDia="0." initWt="4562." len="443." mDiv="10" mFix="1" mStep="-1." massFrac="56.12" mfg="Aerotech" peakThrust="1662.58" propWt="2560." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="221.5" f="0." m="2560." t="0."/>\r
+<eng-data cg="221.5" f="1332.26" m="2545.73" t="0.0386399"/>\r
+<eng-data cg="221.5" f="1563.48" m="2477.47" t="0.123648"/>\r
+<eng-data cg="221.5" f="1519.44" m="2153.77" t="0.502318"/>\r
+<eng-data cg="221.5" f="1574.49" m="1729.48" t="0.996909"/>\r
+<eng-data cg="221.5" f="1662.58" m="1278.61" t="1.49923"/>\r
+<eng-data cg="221.5" f="1574.49" m="827.745" t="2.00155"/>\r
+<eng-data cg="221.5" f="1409.34" m="431.337" t="2.48068"/>\r
+<eng-data cg="221.5" f="1299.23" m="100.518" t="2.92117"/>\r
+<eng-data cg="221.5" f="1167.11" m="52.9487" t="2.99073"/>\r
+<eng-data cg="221.5" f="187.178" m="6.52023" t="3.11437"/>\r
+<eng-data cg="221.5" f="0." m="0." t="3.24"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech L1500T\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-L1500T 98 443 0 2.464 4.6592 AT\r
- 0.073 1320.328\r
- 0.222 1454.823\r
- 0.372 1508.992\r
- 0.522 1556.781\r
- 0.672 1602.407\r
- 0.822 1642.004\r
- 0.971 1670.099\r
- 1.120 1694.804\r
- 1.270 1701.295\r
- 1.420 1704.286\r
- 1.570 1701.008\r
- 1.720 1694.550\r
- 1.869 1683.861\r
- 2.018 1659.694\r
- 2.168 1620.161\r
- 2.318 1570.033\r
- 2.468 1517.933\r
- 2.618 1463.319\r
- 2.767 1400.991\r
- 2.916 1331.420\r
- 3.066 1279.479\r
- 3.216 1108.987\r
- 3.366 217.788\r
- 3.516 10.579\r
- 3.666 3.245\r
- 3.816 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="224.32" Itot="3616.45" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1500.6" burn-time="2.41" cgDiv="10" cgFix="1" cgStep="-1." code="L1500T" delays="1000" dia="98." exitDia="0." initWt="2300." len="665." mDiv="10" mFix="1" mStep="-1." massFrac="71.48" mfg="Aerotech" peakThrust="2381." propWt="1644." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="332.5" f="0." m="1644." t="0."/>\r
+<eng-data cg="332.5" f="1800." m="1562.17" t="0.2"/>\r
+<eng-data cg="332.5" f="2381." m="1277.08" t="0.5"/>\r
+<eng-data cg="332.5" f="2372." m="1266.28" t="0.51"/>\r
+<eng-data cg="332.5" f="1072." m="99.9004" t="2."/>\r
+<eng-data cg="332.5" f="0." m="0." t="2.41"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; Curvefit of Aerotech Instructions by C. Kobel 11/19/08\r
+L2200G 75 665 0-6-10-14-18 2.516 4.751 AT\r
+ 0.011 1195.177\r
+ 0.024 2029.903\r
+ 0.037 2380.868\r
+ 0.050 2542.122\r
+ 0.100 2570.578\r
+ 0.150 2561.093\r
+ 0.200 2523.151\r
+ 0.250 2485.208\r
+ 0.300 2523.151\r
+ 0.350 2570.578\r
+ 0.400 2674.919\r
+ 0.500 2912.057\r
+ 0.600 3073.311\r
+ 0.700 3073.311\r
+ 0.800 3101.768\r
+ 0.900 3092.282\r
+ 1.000 3092.282\r
+ 1.100 2959.485\r
+ 1.186 2807.716\r
+ 1.227 2437.781\r
+ 1.270 2257.556\r
+ 1.300 2162.701\r
+ 1.400 1991.961\r
+ 1.500 1878.135\r
+ 1.600 1792.765\r
+ 1.700 1688.424\r
+ 1.800 1612.54\r
+ 1.900 1584.083\r
+ 2.000 1536.656\r
+ 2.048 1498.714\r
+ 2.084 1403.858\r
+ 2.102 1166.72\r
+ 2.134 796.784\r
+ 2.186 455.305\r
+ 2.237 237.138\r
+ 2.300 94.855\r
+ 2.400 0.0\r
--- /dev/null
+; Entered by Tim Van Milligan. Used John Coker's ThrustCurve Tracer software and\r
+; data supplied by Aerotech thrust stand data. The total weight is a guess.\r
+L339N 98 309 4 1.796 4.5 Aerotech\r
+ 0.049 2.884\r
+ 0.074 373.449\r
+ 0.123 399.403\r
+ 0.156 408.054\r
+ 0.279 415.984\r
+ 0.427 417.426\r
+ 0.476 421.031\r
+ 0.509 416.705\r
+ 0.632 415.984\r
+ 0.837 414.542\r
+ 0.894 418.868\r
+ 0.943 405.17\r
+ 1.026 400.124\r
+ 1.124 402.286\r
+ 1.255 397.961\r
+ 1.362 392.914\r
+ 1.51 391.472\r
+ 1.575 394.356\r
+ 1.592 385.705\r
+ 1.657 387.147\r
+ 1.838 384.984\r
+ 2.026 382.821\r
+ 2.174 379.937\r
+ 2.404 377.053\r
+ 2.478 378.495\r
+ 2.552 377.053\r
+ 2.617 378.495\r
+ 2.683 366.96\r
+ 2.773 359.751\r
+ 2.806 363.355\r
+ 2.937 359.751\r
+ 3.232 351.099\r
+ 3.314 355.425\r
+ 3.356 351.099\r
+ 3.815 345.332\r
+ 3.979 340.285\r
+ 4.233 336.681\r
+ 4.414 333.797\r
+ 4.668 330.913\r
+ 4.996 329.471\r
+ 5.39 323.704\r
+ 5.686 320.099\r
+ 5.989 314.331\r
+ 6.178 310.727\r
+ 6.325 306.401\r
+ 6.514 302.075\r
+ 6.621 302.075\r
+ 6.851 297.75\r
+ 7.195 290.54\r
+ 7.277 293.424\r
+ 7.326 287.656\r
+ 7.441 283.331\r
+ 7.49 286.214\r
+ 7.54 283.331\r
+ 7.696 275.4\r
+ 7.81 273.958\r
+ 7.884 276.842\r
+ 7.942 278.284\r
+ 8.015 276.121\r
+ 8.073 270.354\r
+ 8.188 155.003\r
+ 8.212 118.956\r
+ 8.278 54.071\r
+ 8.311 26.675\r
+ 8.352 7.93\r
+ 8.426 0.0\r
+++ /dev/null
-; AeroTech L850W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-L850W 75 531 0 2.06528 3.67315 AT\r
- 0.091 1015.926\r
- 0.274 1064.942\r
- 0.458 1101.366\r
- 0.643 1143.358\r
- 0.827 1170.928\r
- 1.011 1184.795\r
- 1.196 1178.044\r
- 1.380 1177.598\r
- 1.564 1174.910\r
- 1.748 1170.021\r
- 1.932 1113.716\r
- 2.117 1042.586\r
- 2.301 972.795\r
- 2.485 908.071\r
- 2.670 844.471\r
- 2.854 773.595\r
- 3.039 714.046\r
- 3.222 649.095\r
- 3.406 597.341\r
- 3.591 557.444\r
- 3.775 422.233\r
- 3.959 200.739\r
- 4.144 79.411\r
- 4.328 43.959\r
- 4.513 14.862\r
- 4.697 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="182.44" Itot="3694.98" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="786.668" burn-time="4.7" cgDiv="10" cgFix="1" cgStep="-1." code="L850W" delays="1000" dia="75." exitDia="0." initWt="3673.15" len="531." mDiv="10" mFix="1" mStep="-1." massFrac="56.23" mfg="Aerotech" peakThrust="1184.8" propWt="2065.28" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="265.5" f="0." m="2065.28" t="0."/>\r
+<eng-data cg="265.5" f="1015.93" m="2039.44" t="0.091"/>\r
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+<eng-data cg="265.5" f="1143.36" m="1705.57" t="0.643"/>\r
+<eng-data cg="265.5" f="1170.93" m="1586.56" t="0.827"/>\r
+<eng-data cg="265.5" f="1184.8" m="1465.42" t="1.011"/>\r
+<eng-data cg="265.5" f="1178.04" m="1343.26" t="1.196"/>\r
+<eng-data cg="265.5" f="1177.6" m="1222.12" t="1.38"/>\r
+<eng-data cg="265.5" f="1174.91" m="1101.15" t="1.564"/>\r
+<eng-data cg="265.5" f="1170.02" m="980.569" t="1.748"/>\r
+<eng-data cg="265.5" f="1113.72" m="863.133" t="1.932"/>\r
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+<eng-data cg="265.5" f="972.795" m="648.01" t="2.301"/>\r
+<eng-data cg="265.5" f="908.071" m="551.291" t="2.485"/>\r
+<eng-data cg="265.5" f="844.471" m="460.681" t="2.67"/>\r
+<eng-data cg="265.5" f="773.595" m="377.476" t="2.854"/>\r
+<eng-data cg="265.5" f="714.046" m="300.562" t="3.039"/>\r
+<eng-data cg="265.5" f="649.095" m="230.846" t="3.222"/>\r
+<eng-data cg="265.5" f="597.341" m="166.751" t="3.406"/>\r
+<eng-data cg="265.5" f="557.444" m="107.046" t="3.591"/>\r
+<eng-data cg="265.5" f="422.233" m="56.6687" t="3.775"/>\r
+<eng-data cg="265.5" f="200.739" m="24.6338" t="3.959"/>\r
+<eng-data cg="265.5" f="79.411" m="10.1494" t="4.144"/>\r
+<eng-data cg="265.5" f="43.959" m="3.80542" t="4.328"/>\r
+<eng-data cg="265.5" f="14.862" m="0.764244" t="4.513"/>\r
+<eng-data cg="265.5" f="0." m="0." t="4.697"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech L952W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-L952W 98 427 0 2.73011 5.01222 AT\r
- 0.141 679.073\r
- 0.425 801.562\r
- 0.709 848.474\r
- 0.994 913.345\r
- 1.278 981.614\r
- 1.562 1043.690\r
- 1.847 1088.114\r
- 2.131 1112.556\r
- 2.416 1121.541\r
- 2.700 1118.573\r
- 2.984 1100.665\r
- 3.269 1039.140\r
- 3.553 965.784\r
- 3.837 876.793\r
- 4.122 780.693\r
- 4.406 693.903\r
- 4.691 608.030\r
- 4.975 528.335\r
- 5.259 463.528\r
- 5.544 405.769\r
- 5.828 358.367\r
- 6.112 279.009\r
- 6.397 99.897\r
- 6.681 20.108\r
- 6.967 3.317\r
- 7.252 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="195.43" Itot="5097.92" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="760.884" burn-time="6.7" cgDiv="10" cgFix="1" cgStep="-1." code="L952W" delays="1000" dia="98." exitDia="0." initWt="5026.5" len="443." mDiv="10" mFix="1" mStep="-1." massFrac="52.92" mfg="Aerotech" peakThrust="1056.44" propWt="2660." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="221.5" f="0." m="2660." t="0."/>\r
+<eng-data cg="221.5" f="1.51" m="2660." t="0."/>\r
+<eng-data cg="221.5" f="776.75" m="2639.7" t="0.1"/>\r
+<eng-data cg="221.5" f="909.97" m="2243.65" t="1."/>\r
+<eng-data cg="221.5" f="962.28" m="2097.12" t="1.3"/>\r
+<eng-data cg="221.5" f="1056.44" m="1307.12" t="2.8"/>\r
+<eng-data cg="221.5" f="1047.59" m="1032.66" t="3.3"/>\r
+<eng-data cg="221.5" f="1034.25" m="978.343" t="3.4"/>\r
+<eng-data cg="221.5" f="887.78" m="677.479" t="4."/>\r
+<eng-data cg="221.5" f="519.39" m="200.227" t="5.3"/>\r
+<eng-data cg="221.5" f="288.5" m="52.6869" t="6."/>\r
+<eng-data cg="221.5" f="0." m="0." t="6.7"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; Aerotech M1297W\r
-; Greg Gardner - 12/20/04\r
-M1297W 75 665 0 2.722 4.637 AT\r
-0.10 1433.4\r
-0.15 1789.3\r
-0.20 1922.8\r
-0.25 1869.4\r
-0.30 1856.0\r
-0.35 1833.8\r
-0.40 1767.0\r
-0.50 1722.6\r
-0.60 1709.2\r
-0.90 1700.3\r
-1.00 1688.1\r
-1.50 1678.7\r
-1.75 1634.6\r
-1.85 1622.3\r
-1.95 1572.8\r
-2.00 1554.0\r
-2.50 1346.5\r
-3.00 1136.0\r
-3.20 1053.3\r
-3.25 1044.1\r
-3.35 1032.0\r
-3.38 1020.0\r
-3.40 937.0\r
-3.50 738.0\r
-3.60 545.0\r
-3.75 393.0\r
-4.00 226.0\r
-4.25 94.0\r
-4.35 45.0\r
-4.40 0.0\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="203.79" Itot="5439.04" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1304.33" burn-time="4.17" cgDiv="10" cgFix="1" cgStep="-1." code="M1297W" delays="1000" dia="75." exitDia="0." initWt="4636.8" len="665.48" mDiv="10" mFix="1" mStep="-1." massFrac="58.7" mfg="Aerotech" peakThrust="2047.83" propWt="2721.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="332.74" f="0." m="2721.6" t="0."/>\r
+<eng-data cg="332.74" f="2047.83" m="2706.23" t="0.03"/>\r
+<eng-data cg="332.74" f="1891.3" m="2656.95" t="0.08"/>\r
+<eng-data cg="332.74" f="1734.78" m="2275.92" t="0.5"/>\r
+<eng-data cg="332.74" f="1669.57" m="1850.05" t="1."/>\r
+<eng-data cg="332.74" f="1650." m="1434.79" t="1.5"/>\r
+<eng-data cg="332.74" f="1558.7" m="1033.4" t="2."/>\r
+<eng-data cg="332.74" f="1336.96" m="671.162" t="2.5"/>\r
+<eng-data cg="332.74" f="1115.22" m="364.405" t="3."/>\r
+<eng-data cg="332.74" f="1069.57" m="162.157" t="3.37"/>\r
+<eng-data cg="332.74" f="710.87" m="95.3393" t="3.52"/>\r
+<eng-data cg="332.74" f="489.13" m="71.321" t="3.6"/>\r
+<eng-data cg="332.74" f="182.61" m="9.13748" t="3.97"/>\r
+<eng-data cg="332.74" f="0." m="0." t="4.17"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech M1315W\r
-; Copyright Tripoli Motor Testing 1999 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-M1315W 75 801 0 3.4496 5.6448 AT\r
- 0.116 1728.683\r
- 0.349 1673.336\r
- 0.582 1686.810\r
- 0.816 1696.068\r
- 1.049 1663.167\r
- 1.282 1631.243\r
- 1.516 1620.471\r
- 1.749 1619.702\r
- 1.982 1621.042\r
- 2.216 1615.320\r
- 2.449 1567.089\r
- 2.682 1493.722\r
- 2.916 1420.079\r
- 3.149 1358.660\r
- 3.382 1292.507\r
- 3.616 1224.806\r
- 3.849 1171.995\r
- 4.082 928.809\r
- 4.316 577.949\r
- 4.549 395.445\r
- 4.782 314.006\r
- 5.016 228.273\r
- 5.249 159.803\r
- 5.482 118.348\r
- 5.716 109.782\r
- 5.949 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="196.44" Itot="6645.35" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1117.05" burn-time="5.95" cgDiv="10" cgFix="1" cgStep="-1." code="M1315W" delays="1000" dia="75." exitDia="0." initWt="5644.8" len="801." mDiv="10" mFix="1" mStep="-1." massFrac="61.11" mfg="Aerotech" peakThrust="1728.68" propWt="3449.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="400.5" f="0." m="3449.6" t="0."/>\r
+<eng-data cg="400.5" f="1728.68" m="3397.55" t="0.116"/>\r
+<eng-data cg="400.5" f="1673.34" m="3191.82" t="0.349"/>\r
+<eng-data cg="400.5" f="1686.81" m="2988.61" t="0.582"/>\r
+<eng-data cg="400.5" f="1696.07" m="2783.15" t="0.816"/>\r
+<eng-data cg="400.5" f="1663.17" m="2580." t="1.049"/>\r
+<eng-data cg="400.5" f="1631.24" m="2380.77" t="1.282"/>\r
+<eng-data cg="400.5" f="1620.47" m="2183.28" t="1.516"/>\r
+<eng-data cg="400.5" f="1619.7" m="1987.33" t="1.749"/>\r
+<eng-data cg="400.5" f="1621.04" m="1791.35" t="1.982"/>\r
+<eng-data cg="400.5" f="1615.32" m="1594.79" t="2.216"/>\r
+<eng-data cg="400.5" f="1567.09" m="1402.33" t="2.449"/>\r
+<eng-data cg="400.5" f="1493.72" m="1217.23" t="2.682"/>\r
+<eng-data cg="400.5" f="1420.08" m="1040.26" t="2.916"/>\r
+<eng-data cg="400.5" f="1358.66" m="872.214" t="3.149"/>\r
+<eng-data cg="400.5" f="1292.51" m="711.884" t="3.382"/>\r
+<eng-data cg="400.5" f="1224.81" m="558.995" t="3.616"/>\r
+<eng-data cg="400.5" f="1171.99" m="414.049" t="3.849"/>\r
+<eng-data cg="400.5" f="928.809" m="287.003" t="4.082"/>\r
+<eng-data cg="400.5" f="577.949" m="195.49" t="4.316"/>\r
+<eng-data cg="400.5" f="395.445" m="136.624" t="4.549"/>\r
+<eng-data cg="400.5" f="314.006" m="93.7198" t="4.782"/>\r
+<eng-data cg="400.5" f="228.273" m="60.7847" t="5.016"/>\r
+<eng-data cg="400.5" f="159.803" m="37.3157" t="5.249"/>\r
+<eng-data cg="400.5" f="118.348" m="20.4945" t="5.482"/>\r
+<eng-data cg="400.5" f="109.782" m="6.63908" t="5.716"/>\r
+<eng-data cg="400.5" f="0." m="0." t="5.949"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech M1419W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-M1419W 98 579 0 4.032 6.91622 AT\r
- 0.154 1154.896\r
- 0.465 1241.151\r
- 0.776 1300.224\r
- 1.087 1358.364\r
- 1.399 1411.033\r
- 1.710 1461.033\r
- 2.022 1485.747\r
- 2.333 1503.653\r
- 2.644 1513.113\r
- 2.955 1511.947\r
- 3.267 1492.438\r
- 3.578 1418.368\r
- 3.890 1326.608\r
- 4.201 1219.222\r
- 4.513 1087.648\r
- 4.824 937.068\r
- 5.135 810.066\r
- 5.446 709.130\r
- 5.757 624.701\r
- 6.069 557.223\r
- 6.380 437.806\r
- 6.692 252.076\r
- 7.003 107.741\r
- 7.315 19.973\r
- 7.626 0.515\r
- 7.937 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="193.79" Itot="7582.66" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1083.24" burn-time="7." cgDiv="10" cgFix="1" cgStep="-1." code="M1419W" delays="1000" dia="98." exitDia="0." initWt="6930.7" len="597." mDiv="10" mFix="1" mStep="-1." massFrac="57.57" mfg="Aerotech" peakThrust="1462.23" propWt="3990." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="298.5" f="0." m="3990." t="0."/>\r
+<eng-data cg="298.5" f="0.22" m="3990." t="0."/>\r
+<eng-data cg="298.5" f="1307.13" m="3955.6" t="0.1"/>\r
+<eng-data cg="298.5" f="1218.53" m="3889.15" t="0.2"/>\r
+<eng-data cg="298.5" f="1373.59" m="3070.77" t="1.4"/>\r
+<eng-data cg="298.5" f="1462.23" m="2250.05" t="2.5"/>\r
+<eng-data cg="298.5" f="1440.04" m="1868.26" t="3."/>\r
+<eng-data cg="298.5" f="1404.63" m="1419.2" t="3.6"/>\r
+<eng-data cg="298.5" f="1160.84" m="879.219" t="4.4"/>\r
+<eng-data cg="298.5" f="664.66" m="206.814" t="5.8"/>\r
+<eng-data cg="298.5" f="629.17" m="104.692" t="6.1"/>\r
+<eng-data cg="298.5" f="177.25" m="19.8246" t="6.5"/>\r
+<eng-data cg="298.5" f="8.9" m="0.234159" t="6.9"/>\r
+<eng-data cg="298.5" f="0." m="0." t="7."/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+; Curvefit of AeroTech Instructions by C. Kobel 11/19/08\r
+M1500G 75 665 0-6-10-14-18 2.631 4.896 AT\r
+ 0.012 1183.8\r
+ 0.023 1614.273\r
+ 0.050 1694.987\r
+ 0.100 1716.511\r
+ 0.150 1694.987\r
+ 0.200 1603.512\r
+ 0.250 1517.417\r
+ 0.300 1490.512\r
+ 0.400 1474.37\r
+ 0.500 1485.132\r
+ 0.600 1512.036\r
+ 0.700 1533.56\r
+ 0.800 1571.226\r
+ 0.900 1608.892\r
+ 1.000 1630.416\r
+ 1.100 1657.321\r
+ 1.200 1684.225\r
+ 1.300 1694.987\r
+ 1.400 1694.987\r
+ 1.500 1700.368\r
+ 1.600 1700.368\r
+ 1.700 1705.749\r
+ 1.800 1689.606\r
+ 1.900 1662.702\r
+ 2.000 1657.321\r
+ 2.100 1608.892\r
+ 2.200 1581.988\r
+ 2.300 1555.083\r
+ 2.400 1522.798\r
+ 2.500 1490.512\r
+ 2.600 1463.608\r
+ 2.700 1431.322\r
+ 2.800 1415.18\r
+ 2.900 1388.275\r
+ 3.000 1361.371\r
+ 3.100 1372.132\r
+ 3.200 1286.038\r
+ 3.250 1226.848\r
+ 3.300 973.945\r
+ 3.400 478.901\r
+ 3.450 220.617\r
+ 3.500 80.714\r
+ 3.600 0.0\r
+++ /dev/null
-; AeroTech M1550R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-M1550R 75 800 0 3.4496 5.6448 AT\r
- 0.069 1720.759\r
- 0.212 2125.329\r
- 0.358 1995.947\r
- 0.501 1908.442\r
- 0.645 1868.713\r
- 0.790 1835.504\r
- 0.935 1808.662\r
- 1.079 1796.300\r
- 1.222 1785.423\r
- 1.368 1773.153\r
- 1.511 1746.590\r
- 1.655 1715.709\r
- 1.800 1689.633\r
- 1.945 1660.720\r
- 2.089 1633.277\r
- 2.232 1606.038\r
- 2.378 1570.222\r
- 2.521 1534.714\r
- 2.665 1503.345\r
- 2.810 1461.317\r
- 2.955 1427.572\r
- 3.099 1393.229\r
- 3.242 939.955\r
- 3.388 268.504\r
- 3.532 4.985\r
- 3.677 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="161.41" Itot="5529.12" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1531.61" burn-time="3.61" cgDiv="10" cgFix="1" cgStep="-1." code="M1550R" delays="1000" dia="75." exitDia="0." initWt="5715." len="800." mDiv="10" mFix="1" mStep="-1." massFrac="61.12" mfg="Aerotech" peakThrust="2125.33" propWt="3493." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="400." f="0." m="3493." t="0."/>\r
+<eng-data cg="400." f="1720.76" m="3454.95" t="0.07"/>\r
+<eng-data cg="400." f="2125.33" m="3284.87" t="0.21"/>\r
+<eng-data cg="400." f="1995.95" m="3089.6" t="0.36"/>\r
+<eng-data cg="400." f="1908.44" m="2916.94" t="0.5"/>\r
+<eng-data cg="400." f="1868.71" m="2737.97" t="0.65"/>\r
+<eng-data cg="400." f="1835.5" m="2574.16" t="0.79"/>\r
+<eng-data cg="400." f="1808.66" m="2401.5" t="0.94"/>\r
+<eng-data cg="400." f="1796.3" m="2242.08" t="1.08"/>\r
+<eng-data cg="400." f="1785.42" m="2083.69" t="1.22"/>\r
+<eng-data cg="400." f="1773.15" m="1915.08" t="1.37"/>\r
+<eng-data cg="400." f="1746.59" m="1759.43" t="1.51"/>\r
+<eng-data cg="400." f="1715.71" m="1595.38" t="1.66"/>\r
+<eng-data cg="400." f="1689.63" m="1444.79" t="1.8"/>\r
+<eng-data cg="400." f="1660.72" m="1286.05" t="1.95"/>\r
+<eng-data cg="400." f="1633.28" m="1140.38" t="2.09"/>\r
+<eng-data cg="400." f="1606.04" m="997.13" t="2.23"/>\r
+<eng-data cg="400." f="1570.22" m="846.636" t="2.38"/>\r
+<eng-data cg="400." f="1534.71" m="709.329" t="2.52"/>\r
+<eng-data cg="400." f="1503.35" m="565.382" t="2.67"/>\r
+<eng-data cg="400." f="1461.32" m="434.278" t="2.81"/>\r
+<eng-data cg="400." f="1427.57" m="297.4" t="2.96"/>\r
+<eng-data cg="400." f="1393.23" m="172.657" t="3.1"/>\r
+<eng-data cg="400." f="939.96" m="69.4785" t="3.24"/>\r
+<eng-data cg="400." f="268.5" m="12.2204" t="3.39"/>\r
+<eng-data cg="400." f="4.99" m="0.126097" t="3.53"/>\r
+<eng-data cg="400." f="0." m="0." t="3.61"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech M1600R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-M1600R 98 579 0 4.032 6.91712 AT\r
- 0.088 1370.361\r
- 0.268 1626.628\r
- 0.448 1672.654\r
- 0.628 1720.596\r
- 0.808 1763.287\r
- 0.987 1801.282\r
- 1.167 1829.825\r
- 1.348 1845.146\r
- 1.529 1856.370\r
- 1.710 1850.089\r
- 1.890 1847.370\r
- 2.070 1829.454\r
- 2.250 1810.982\r
- 2.430 1784.910\r
- 2.610 1754.267\r
- 2.790 1726.898\r
- 2.971 1689.288\r
- 3.152 1641.579\r
- 3.332 1581.589\r
- 3.513 1511.036\r
- 3.692 1431.400\r
- 3.872 1361.032\r
- 4.053 1234.566\r
- 4.232 621.206\r
- 4.414 42.471\r
- 4.595 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="174.7" Itot="6993.2" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1554.04" burn-time="4.5" cgDiv="10" cgFix="1" cgStep="-1." code="M1600R" delays="1000" dia="98." exitDia="0." initWt="7004." len="579." mDiv="10" mFix="1" mStep="-1." massFrac="58.28" mfg="Aerotech" peakThrust="1856.37" propWt="4082." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="289.5" f="0." m="4082." t="0."/>\r
+<eng-data cg="289.5" f="1370.36" m="4046." t="0.09"/>\r
+<eng-data cg="289.5" f="1626.63" m="3888.56" t="0.27"/>\r
+<eng-data cg="289.5" f="1672.65" m="3715.24" t="0.45"/>\r
+<eng-data cg="289.5" f="1720.6" m="3536.98" t="0.63"/>\r
+<eng-data cg="289.5" f="1763.29" m="3353.95" t="0.81"/>\r
+<eng-data cg="289.5" f="1801.28" m="3166.69" t="0.99"/>\r
+<eng-data cg="289.5" f="1829.83" m="2975.94" t="1.17"/>\r
+<eng-data cg="289.5" f="1845.15" m="2782.88" t="1.35"/>\r
+<eng-data cg="289.5" f="1856.37" m="2588.42" t="1.53"/>\r
+<eng-data cg="289.5" f="1850.09" m="2393.71" t="1.71"/>\r
+<eng-data cg="289.5" f="1847.37" m="2199.46" t="1.89"/>\r
+<eng-data cg="289.5" f="1829.45" m="2006.31" t="2.07"/>\r
+<eng-data cg="289.5" f="1810.98" m="1815.06" t="2.25"/>\r
+<eng-data cg="289.5" f="1784.91" m="1626.15" t="2.43"/>\r
+<eng-data cg="289.5" f="1754.27" m="1440.23" t="2.61"/>\r
+<eng-data cg="289.5" f="1726.9" m="1257.35" t="2.79"/>\r
+<eng-data cg="289.5" f="1689.29" m="1077.88" t="2.97"/>\r
+<eng-data cg="289.5" f="1641.58" m="902.898" t="3.15"/>\r
+<eng-data cg="289.5" f="1581.59" m="733.573" t="3.33"/>\r
+<eng-data cg="289.5" f="1511.04" m="571.105" t="3.51"/>\r
+<eng-data cg="289.5" f="1431.4" m="416.527" t="3.69"/>\r
+<eng-data cg="289.5" f="1361.03" m="269.83" t="3.87"/>\r
+<eng-data cg="289.5" f="1234.57" m="133.473" t="4.05"/>\r
+<eng-data cg="289.5" f="621.21" m="35.9813" t="4.23"/>\r
+<eng-data cg="289.5" f="42.47" m="1.11556" t="4.41"/>\r
+<eng-data cg="289.5" f="0." m="0." t="4.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+M1780 98 665 P 2.56 4.715 AT\r
+ 0.028 2204.193\r
+ 0.118 2566.025\r
+ 0.173 2566.025\r
+ 0.341 2214.151\r
+ 0.44 2144.44\r
+ 0.636 2114.564\r
+ 1.34 2134.482\r
+ 1.395 2204.193\r
+ 1.648 2121.203\r
+ 1.841 2041.534\r
+ 1.874 1895.473\r
+ 2.127 1643.186\r
+ 2.353 1517.042\r
+ 2.584 1460.61\r
+ 2.672 1347.744\r
+ 2.763 1068.901\r
+ 2.829 723.666\r
+ 2.939 438.183\r
+ 2.999 292.122\r
+ 3.101 172.617\r
+ 3.272 36.515\r
+ 3.5 0.0\r
--- /dev/null
+; Entered by Tim Van Milligan. Used John Coker's ThrustCurve Tracer software and\r
+; data from TRA certification dated 10-14-08\r
+M1800FJ 98 751 4 5.599 9.162 Aerotech\r
+ 0.021 3007.361\r
+ 0.043 1964.715\r
+ 0.059 1858.322\r
+ 0.069 1766.116\r
+ 0.134 1829.951\r
+ 0.192 1822.858\r
+ 0.267 1822.858\r
+ 0.363 1865.415\r
+ 0.502 1936.344\r
+ 0.582 1922.158\r
+ 0.684 1964.715\r
+ 1.132 2071.107\r
+ 1.581 2149.129\r
+ 1.923 2198.778\r
+ 2.142 2220.057\r
+ 2.393 2220.057\r
+ 2.463 2198.778\r
+ 2.655 2106.572\r
+ 2.831 2007.272\r
+ 2.922 1978.901\r
+ 3.029 1915.065\r
+ 3.21 1808.673\r
+ 3.349 1695.187\r
+ 3.526 1588.795\r
+ 3.723 1439.845\r
+ 3.851 1397.288\r
+ 3.921 1361.824\r
+ 4.017 1255.432\r
+ 4.097 1120.668\r
+ 4.167 978.811\r
+ 4.263 780.212\r
+ 4.327 624.169\r
+ 4.402 453.941\r
+ 4.428 375.92\r
+ 4.482 276.621\r
+ 4.53 177.321\r
+ 4.583 99.3\r
+ 4.653 42.557\r
+ 4.76 21.279\r
+ 4.952 0.0\r
--- /dev/null
+M1845 98 597 P 3.7720000000000002 6.682 AT\r
+ 0.024 2261.638\r
+ 0.067 2115.94\r
+ 1.032 2268.261\r
+ 1.354 2433.828\r
+ 2.253 2288.129\r
+ 2.406 2149.053\r
+ 2.578 1821.232\r
+ 3.065 1579.504\r
+ 3.583 1410.627\r
+ 3.838 1364.268\r
+ 3.913 1218.569\r
+ 3.995 685.445\r
+ 4.109 400.671\r
+ 4.352 248.35\r
+ 4.498 33.113\r
+ 4.729 0.0\r
+++ /dev/null
-; AeroTech M1939W\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-M1939W 98 732 0 5.656 8.98822 AT\r
- 0.134 1905.185\r
- 0.406 2021.155\r
- 0.679 2095.900\r
- 0.952 2158.087\r
- 1.225 2198.211\r
- 1.498 2219.694\r
- 1.770 2228.643\r
- 2.042 2229.881\r
- 2.315 2225.641\r
- 2.587 2211.713\r
- 2.860 2164.724\r
- 3.133 2047.014\r
- 3.405 1916.238\r
- 3.677 1805.664\r
- 3.950 1658.489\r
- 4.223 1497.704\r
- 4.496 1339.452\r
- 4.769 1213.061\r
- 5.041 1102.130\r
- 5.313 966.508\r
- 5.585 670.253\r
- 5.858 443.975\r
- 6.131 155.355\r
- 6.404 41.358\r
- 6.677 5.775\r
- 6.950 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="198.19" Itot="10339.8" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1477.12" burn-time="7." cgDiv="10" cgFix="1" cgStep="-1." code="M1939W" delays="1000" dia="98." exitDia="0." initWt="8844.5" len="751." mDiv="10" mFix="1" mStep="-1." massFrac="60.15" mfg="Aerotech" peakThrust="2084.16" propWt="5320." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="375.5" f="0." m="5320." t="0."/>\r
+<eng-data cg="375.5" f="1.33" m="5320." t="0."/>\r
+<eng-data cg="375.5" f="1806.56" m="5273.49" t="0.1"/>\r
+<eng-data cg="375.5" f="1881.42" m="4799.11" t="0.6"/>\r
+<eng-data cg="375.5" f="1982.79" m="4103.24" t="1.3"/>\r
+<eng-data cg="375.5" f="2062.09" m="3478.89" t="1.9"/>\r
+<eng-data cg="375.5" f="2079.71" m="3265.79" t="2.1"/>\r
+<eng-data cg="375.5" f="2084.16" m="2730.2" t="2.6"/>\r
+<eng-data cg="375.5" f="1982.79" m="1997.82" t="3.3"/>\r
+<eng-data cg="375.5" f="1696.38" m="1240.62" t="4.1"/>\r
+<eng-data cg="375.5" f="1145.58" m="436.393" t="5.2"/>\r
+<eng-data cg="375.5" f="991.37" m="216.494" t="5.6"/>\r
+<eng-data cg="375.5" f="176.23" m="36.2693" t="6.2"/>\r
+<eng-data cg="375.5" f="0." m="0." t="7."/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech M2000R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-M2000R 98 732 0 5.65824 8.98688 AT\r
- 0.091 1530.959\r
- 0.279 2186.270\r
- 0.466 2166.698\r
- 0.655 2187.237\r
- 0.844 2219.069\r
- 1.031 2248.071\r
- 1.220 2273.743\r
- 1.409 2298.306\r
- 1.596 2309.753\r
- 1.785 2315.708\r
- 1.974 2316.158\r
- 2.161 2306.313\r
- 2.350 2282.230\r
- 2.539 2252.104\r
- 2.726 2209.638\r
- 2.915 2168.800\r
- 3.104 2117.175\r
- 3.291 2067.533\r
- 3.480 2004.508\r
- 3.669 1934.442\r
- 3.856 1831.480\r
- 4.045 1745.634\r
- 4.234 1504.269\r
- 4.421 649.796\r
- 4.610 58.178\r
- 4.799 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="163.42" Itot="9181.04" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1953.41" burn-time="4.7" cgDiv="10" cgFix="1" cgStep="-1." code="M2000R" delays="1000" dia="98." exitDia="0." initWt="9099." len="732." mDiv="10" mFix="1" mStep="-1." massFrac="62.96" mfg="Aerotech" peakThrust="2316.16" propWt="5729." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="366." f="0." m="5729." t="0."/>\r
+<eng-data cg="366." f="1530.96" m="5686.01" t="0.09"/>\r
+<eng-data cg="366." f="2186.27" m="5465.65" t="0.28"/>\r
+<eng-data cg="366." f="2166.7" m="5207.61" t="0.47"/>\r
+<eng-data cg="366." f="2187.24" m="4949.5" t="0.66"/>\r
+<eng-data cg="366." f="2219.07" m="4702.04" t="0.84"/>\r
+<eng-data cg="366." f="2248.07" m="4437.23" t="1.03"/>\r
+<eng-data cg="366." f="2273.74" m="4169.18" t="1.22"/>\r
+<eng-data cg="366." f="2298.31" m="3898.14" t="1.41"/>\r
+<eng-data cg="366." f="2309.75" m="3624.98" t="1.6"/>\r
+<eng-data cg="366." f="2315.71" m="3365.21" t="1.78"/>\r
+<eng-data cg="366." f="2316.16" m="3090.63" t="1.97"/>\r
+<eng-data cg="366." f="2306.31" m="2816.61" t="2.16"/>\r
+<eng-data cg="366." f="2282.23" m="2544.6" t="2.35"/>\r
+<eng-data cg="366." f="2252.1" m="2275.8" t="2.54"/>\r
+<eng-data cg="366." f="2209.64" m="2011.31" t="2.73"/>\r
+<eng-data cg="366." f="2168.8" m="1751.75" t="2.92"/>\r
+<eng-data cg="366." f="2117.18" m="1511.05" t="3.1"/>\r
+<eng-data cg="366." f="2067.53" m="1262.98" t="3.29"/>\r
+<eng-data cg="366." f="2004.51" m="1021.59" t="3.48"/>\r
+<eng-data cg="366." f="1934.44" m="788.088" t="3.67"/>\r
+<eng-data cg="366." f="1831.48" m="564.843" t="3.86"/>\r
+<eng-data cg="366." f="1745.63" m="363.952" t="4.04"/>\r
+<eng-data cg="366." f="1504.27" m="171.297" t="4.23"/>\r
+<eng-data cg="366." f="649.8" m="43.603" t="4.42"/>\r
+<eng-data cg="366." f="58.18" m="1.6337" t="4.61"/>\r
+<eng-data cg="366." f="0." m="0." t="4.7"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Aerotech" code="M2030G" Type="reloadable" dia="75." len="653."\r
+initWt="4906." propWt="2663." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="2002.58" peakThrust="2645.93" throatDia="0." exitDia="0."\r
+Itot="5356.89" burn-time="2.67" massFrac="54.28" Isp="205.13" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Took this data from the Aerotech Typical Time-Thrust Curve that comes with the M2030G motor.</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="2663." cg="326.5"/>\r
+ <eng-data t="0.00776398" f="1342.14" m="2660.41" cg="326.5"/>\r
+ <eng-data t="0.0776398" f="2147.42" m="2599.8" cg="326.5"/>\r
+ <eng-data t="0.15528" f="1840.64" m="2522.84" cg="326.5"/>\r
+ <eng-data t="0.496894" f="2224.11" m="2177.7" cg="326.5"/>\r
+ <eng-data t="0.784161" f="2607.58" m="1832.7" cg="326.5"/>\r
+ <eng-data t="1.00155" f="2645.93" m="1548.83" cg="326.5"/>\r
+ <eng-data t="1.3587" f="2530.88" m="1089.28" cg="326.5"/>\r
+ <eng-data t="1.49068" f="2415.84" m="926.996" cg="326.5"/>\r
+ <eng-data t="1.99534" f="1802.3" m="397.884" cg="326.5"/>\r
+ <eng-data t="2.3913" f="1418.83" m="80.8616" cg="326.5"/>\r
+ <eng-data t="2.5" f="805.282" m="20.7723" cg="326.5"/>\r
+ <eng-data t="2.56211" f="191.734" m="5.37992" cg="326.5"/>\r
+ <eng-data t="2.675" f="0." m="0." cg="326.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; Entered by Tim Van Milligan for RockSim Users. Used John Coker's ThrustCurve\r
+; Tracer software and TRA cert paperwork dated 10-14-08.\r
+M2100G 98 597 4 4.03 7.03 Aerotech\r
+ 0.014 72.789\r
+ 0.017 1148.45\r
+ 0.021 1552.833\r
+ 0.038 1593.272\r
+ 0.042 1908.691\r
+ 0.052 2062.357\r
+ 0.077 2151.321\r
+ 0.115 2207.935\r
+ 0.167 2240.285\r
+ 0.223 2256.461\r
+ 0.272 2256.461\r
+ 0.31 2232.198\r
+ 0.415 2280.724\r
+ 0.59 2385.863\r
+ 0.701 2410.126\r
+ 0.876 2507.179\r
+ 0.959 2555.705\r
+ 1.043 2588.055\r
+ 1.176 2677.02\r
+ 1.263 2782.159\r
+ 1.333 2830.685\r
+ 1.437 2846.861\r
+ 1.517 2879.211\r
+ 1.608 2968.176\r
+ 1.667 2943.913\r
+ 1.81 2935.825\r
+ 1.926 2895.387\r
+ 1.999 2846.861\r
+ 2.041 2782.159\r
+ 2.152 2531.442\r
+ 2.393 1949.129\r
+ 2.484 1787.376\r
+ 2.56 1674.148\r
+ 2.738 1504.307\r
+ 2.836 1439.606\r
+ 2.958 1366.817\r
+ 3.091 1285.94\r
+ 3.178 1229.326\r
+ 3.23 1196.976\r
+ 3.283 1180.8\r
+ 3.401 1188.888\r
+ 3.447 1140.362\r
+ 3.478 1035.222\r
+ 3.513 913.907\r
+ 3.516 541.874\r
+ 3.527 444.822\r
+ 3.541 0.0\r
+++ /dev/null
-; AeroTech M2400T\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-M2400T 98 597 0 3.65254 6.4512 AT\r
- 0.070 2441.945\r
- 0.211 2495.460\r
- 0.353 2556.133\r
- 0.495 2601.596\r
- 0.636 2637.660\r
- 0.778 2660.804\r
- 0.920 2676.486\r
- 1.061 2687.081\r
- 1.203 2695.807\r
- 1.345 2694.493\r
- 1.486 2684.268\r
- 1.628 2667.289\r
- 1.771 2629.961\r
- 1.914 2578.923\r
- 2.055 2522.074\r
- 2.197 2461.704\r
- 2.339 2393.518\r
- 2.480 2303.939\r
- 2.622 2201.610\r
- 2.764 2097.461\r
- 2.905 2010.409\r
- 3.047 1275.776\r
- 3.189 418.836\r
- 3.330 17.586\r
- 3.473 3.669\r
- 3.616 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="210.42" Itot="7619.76" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2177.07" burn-time="3.5" cgDiv="10" cgFix="1" cgStep="-1." code="M2400T" delays="1000" dia="98." exitDia="0." initWt="6483." len="597." mDiv="10" mFix="1" mStep="-1." massFrac="56.96" mfg="Aerotech" peakThrust="3237.07" propWt="3692.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="298.5" f="0." m="3692.6" t="0."/>\r
+<eng-data cg="298.5" f="3237.07" m="3674.42" t="0.0231839"/>\r
+<eng-data cg="298.5" f="2356.24" m="3653.47" t="0.0386399"/>\r
+<eng-data cg="298.5" f="2576.45" m="3625.76" t="0.0618238"/>\r
+<eng-data cg="298.5" f="2356.24" m="3598.05" t="0.0850077"/>\r
+<eng-data cg="298.5" f="2532.4" m="3295.96" t="0.340031"/>\r
+<eng-data cg="298.5" f="2708.57" m="2275.33" t="1.14374"/>\r
+<eng-data cg="298.5" f="2642.51" m="1784.35" t="1.52241"/>\r
+<eng-data cg="298.5" f="2532.4" m="1173.87" t="2.00927"/>\r
+<eng-data cg="298.5" f="2313.08" m="593.185" t="2.50386"/>\r
+<eng-data cg="298.5" f="2025.92" m="211.311" t="2.86708"/>\r
+<eng-data cg="298.5" f="1519.44" m="98.457" t="2.99845"/>\r
+<eng-data cg="298.5" f="198.188" m="14.8323" t="3.19938"/>\r
+<eng-data cg="298.5" f="66.0627" m="1.47203" t="3.40804"/>\r
+<eng-data cg="298.5" f="0." m="0." t="3.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; AeroTech M2500T\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-M2500T 98 751 0 4.6592 8.064 AT\r
- 0.082 2651.855\r
- 0.249 2780.285\r
- 0.416 2820.733\r
- 0.583 2843.010\r
- 0.751 2847.765\r
- 0.918 2851.215\r
- 1.084 2854.737\r
- 1.252 2861.690\r
- 1.420 2858.088\r
- 1.586 2851.086\r
- 1.754 2844.622\r
- 1.922 2830.855\r
- 2.089 2804.711\r
- 2.255 2765.796\r
- 2.423 2710.509\r
- 2.591 2648.262\r
- 2.757 2586.910\r
- 2.925 2520.794\r
- 3.093 2462.217\r
- 3.259 2419.937\r
- 3.426 1894.936\r
- 3.594 808.043\r
- 3.761 282.403\r
- 3.928 97.876\r
- 4.096 24.492\r
- 4.264 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="209.52" Itot="9573." Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2245.07" burn-time="4.26" cgDiv="10" cgFix="1" cgStep="-1." code="M2500T" delays="1000" dia="98." exitDia="0." initWt="8064." len="751." mDiv="10" mFix="1" mStep="-1." massFrac="57.78" mfg="Aerotech" peakThrust="2861.69" propWt="4659.2" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AeroTech M2500T\r
+Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
+provided by ThrustCurve.org (www.thrustcurve.org)\r
+</comments>\r
+<data>\r
+<eng-data cg="375.5" f="0." m="4659.2" t="0."/>\r
+<eng-data cg="375.5" f="2651.86" m="4606.28" t="0.082"/>\r
+<eng-data cg="375.5" f="2780.28" m="4385.52" t="0.249"/>\r
+<eng-data cg="375.5" f="2820.73" m="4157.9" t="0.416"/>\r
+<eng-data cg="375.5" f="2843.01" m="3927.73" t="0.583"/>\r
+<eng-data cg="375.5" f="2847.76" m="3695.07" t="0.751"/>\r
+<eng-data cg="375.5" f="2851.22" m="3463.47" t="0.918"/>\r
+<eng-data cg="375.5" f="2854.74" m="3232.97" t="1.084"/>\r
+<eng-data cg="375.5" f="2861.69" m="2999.26" t="1.252"/>\r
+<eng-data cg="375.5" f="2858.09" m="2765.42" t="1.42"/>\r
+<eng-data cg="375.5" f="2851.09" m="2534.79" t="1.586"/>\r
+<eng-data cg="375.5" f="2844.62" m="2301.93" t="1.754"/>\r
+<eng-data cg="375.5" f="2830.86" m="2069.9" t="1.922"/>\r
+<eng-data cg="375.5" f="2804.71" m="1840.87" t="2.089"/>\r
+<eng-data cg="375.5" f="2765.8" m="1615.85" t="2.255"/>\r
+<eng-data cg="375.5" f="2710.51" m="1391.96" t="2.423"/>\r
+<eng-data cg="375.5" f="2648.26" m="1172.88" t="2.591"/>\r
+<eng-data cg="375.5" f="2586.91" m="961.395" t="2.757"/>\r
+<eng-data cg="375.5" f="2520.79" m="752.577" t="2.925"/>\r
+<eng-data cg="375.5" f="2462.22" m="548.856" t="3.093"/>\r
+<eng-data cg="375.5" f="2419.94" m="351.635" t="3.259"/>\r
+<eng-data cg="375.5" f="1894.94" m="176.28" t="3.426"/>\r
+<eng-data cg="375.5" f="808.043" m="65.7738" t="3.594"/>\r
+<eng-data cg="375.5" f="282.403" m="21.4585" t="3.761"/>\r
+<eng-data cg="375.5" f="97.876" m="6.00408" t="3.928"/>\r
+<eng-data cg="375.5" f="24.492" m="1.00131" t="4.096"/>\r
+<eng-data cg="375.5" f="0." m="0." t="4.264"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;75-6400 case\r
-; Greg Gardner - 10/25/07\r
-M650W 75 801 0 3.351 5.125 AT\r
-0.08 1240\r
-0.12 1328\r
-0.25 1230\r
-0.5 1142\r
-1.0 1071\r
-1.5 1048\r
-2.0 1018\r
-2.5 982\r
-3.0 950\r
-3.5 853\r
-4.0 781\r
-5.0 595\r
-6.0 443\r
-7.0 297\r
-8.0 155\r
-9.0 88\r
-10.0 32\r
-10.5 12\r
-11.0 4\r
-11.5 0\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="182.76" Itot="6005.98" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="522.259" burn-time="11.5" cgDiv="10" cgFix="1" cgStep="-1." code="M650W" delays="1000" dia="75." exitDia="0." initWt="5125." len="801." mDiv="10" mFix="1" mStep="-1." massFrac="65.39" mfg="AT" peakThrust="1328." propWt="3351." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>75-6400 case\r
+Greg Gardner - 10/25/07\r
+</comments>\r
+<data>\r
+<eng-data cg="400.5" f="0." m="3351." t="0."/>\r
+<eng-data cg="400.5" f="1240." m="3323.33" t="0.08"/>\r
+<eng-data cg="400.5" f="1328." m="3294.67" t="0.12"/>\r
+<eng-data cg="400.5" f="1230." m="3201.9" t="0.25"/>\r
+<eng-data cg="400.5" f="1142." m="3036.47" t="0.5"/>\r
+<eng-data cg="400.5" f="1071." m="2727.79" t="1."/>\r
+<eng-data cg="400.5" f="1048." m="2432.22" t="1.5"/>\r
+<eng-data cg="400.5" f="1018." m="2144.04" t="2."/>\r
+<eng-data cg="400.5" f="982." m="1865.07" t="2.5"/>\r
+<eng-data cg="400.5" f="950." m="1595.58" t="3."/>\r
+<eng-data cg="400.5" f="853." m="1344.09" t="3.5"/>\r
+<eng-data cg="400.5" f="781." m="1116.17" t="4."/>\r
+<eng-data cg="400.5" f="595." m="732.301" t="5."/>\r
+<eng-data cg="400.5" f="443." m="442.728" t="6."/>\r
+<eng-data cg="400.5" f="297." m="236.289" t="7."/>\r
+<eng-data cg="400.5" f="155." m="110.194" t="8."/>\r
+<eng-data cg="400.5" f="88." m="42.4037" t="9."/>\r
+<eng-data cg="400.5" f="32." m="8.9271" t="10."/>\r
+<eng-data cg="400.5" f="12." m="2.78972" t="10.5"/>\r
+<eng-data cg="400.5" f="4." m="0.557944" t="11."/>\r
+<eng-data cg="400.5" f="0." m="0." t="11.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;98-10240 case\r
-; Greg Gardner - 10/25/07\r
-M750W 98 732 0 5.3 8.776 AT\r
-0.1 1032\r
-0.2 992\r
-0.3 974\r
-0.48 966\r
-1.0 1055\r
-1.5 1152\r
-2.0 1192\r
-2.5 1218\r
-4.0 1103\r
-6.0 818\r
-8.0 561\r
-10.0 318\r
-11.0 216\r
-12.0 125\r
-13.0 76\r
-14.0 47\r
-15.0 23\r
-15.5 9\r
-16.0 0\r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="178.08" Itot="9255.91" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="578.494" burn-time="16." cgDiv="10" cgFix="1" cgStep="-1." code="M750W" delays="1000" dia="98." exitDia="0." initWt="8776." len="732." mDiv="10" mFix="1" mStep="-1." massFrac="60.39" mfg="Aerotech" peakThrust="1218." propWt="5300." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>98-10240 case\r
+Greg Gardner - 10/25/07\r
+</comments>\r
+<data>\r
+<eng-data cg="366." f="0." m="5300." t="0."/>\r
+<eng-data cg="366." f="1032." m="5270.45" t="0.1"/>\r
+<eng-data cg="366." f="992." m="5212.51" t="0.2"/>\r
+<eng-data cg="366." f="974." m="5156.22" t="0.3"/>\r
+<eng-data cg="366." f="966." m="5056.24" t="0.48"/>\r
+<eng-data cg="366." f="1055." m="4755.36" t="1."/>\r
+<eng-data cg="366." f="1152." m="4439.42" t="1.5"/>\r
+<eng-data cg="366." f="1192." m="4103.88" t="2."/>\r
+<eng-data cg="366." f="1218." m="3758.88" t="2.5"/>\r
+<eng-data cg="366." f="1103." m="2762.11" t="4."/>\r
+<eng-data cg="366." f="818." m="1662.14" t="6."/>\r
+<eng-data cg="366." f="561." m="872.51" t="8."/>\r
+<eng-data cg="366." f="318." m="369.188" t="10."/>\r
+<eng-data cg="366." f="216." m="216.302" t="11."/>\r
+<eng-data cg="366." f="125." m="118.673" t="12."/>\r
+<eng-data cg="366." f="76." m="61.1258" t="13."/>\r
+<eng-data cg="366." f="47." m="25.9105" t="14."/>\r
+<eng-data cg="366." f="23." m="5.86922" t="15."/>\r
+<eng-data cg="366." f="9." m="1.28837" t="15.5"/>\r
+<eng-data cg="366." f="0." m="0." t="16."/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-M845HW 98 795.02 100 3.569 6.833 AT\r
-0.015456 1332.26\r
-0.0463679 1706.62\r
-0.0772798 1178.12\r
-0.185471 1310.24\r
-0.973725 1222.16\r
-1.51468 1200.14\r
-1.97836 1123.07\r
-3.97218 1057\r
-4.20402 880.836\r
-6.01236 627.596\r
-6.495 418.397\r
-7.017 99.0941\r
-7.5 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="188.62" Itot="6601.6" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="880.213" burn-time="7.5" cgDiv="10" cgFix="1" cgStep="-1." code="M845HW" delays="1000" dia="98." exitDia="0." initWt="6833." len="795.02" mDiv="10" mFix="1" mStep="-1." massFrac="52.23" mfg="Aerotech" peakThrust="1706.62" propWt="3569." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="397.51" f="0." m="3569." t="0."/>\r
+<eng-data cg="397.51" f="1332.26" m="3563.43" t="0.015456"/>\r
+<eng-data cg="397.51" f="1706.62" m="3538.04" t="0.0463679"/>\r
+<eng-data cg="397.51" f="1178.12" m="3513.94" t="0.0772798"/>\r
+<eng-data cg="397.51" f="1310.24" m="3441.16" t="0.185471"/>\r
+<eng-data cg="397.51" f="1222.16" m="2901.57" t="0.973725"/>\r
+<eng-data cg="397.51" f="1200.14" m="2547.36" t="1.51468"/>\r
+<eng-data cg="397.51" f="1123.07" m="2256.18" t="1.97836"/>\r
+<eng-data cg="397.51" f="1057." m="1081.21" t="3.97218"/>\r
+<eng-data cg="397.51" f="880.836" m="959.771" t="4.20402"/>\r
+<eng-data cg="397.51" f="627.596" m="222.422" t="6.01236"/>\r
+<eng-data cg="397.51" f="418.397" m="85.9577" t="6.495"/>\r
+<eng-data cg="397.51" f="99.0941" m="12.9379" t="7.017"/>\r
+<eng-data cg="397.51" f="0." m="0." t="7.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+; @TI: 14137.65, @TIa: 14071.08, @TIe: 0.0%, @ThMax: 2137.42, @ThAvg: 1048.203, @Tb: 13.424\r
+; Exported using ThrustCurveTool, www.ThrustGear.com\r
+N1048 98 1046 P 7.925 12.777 AT/RCS\r
+0.0 0.457288\r
+0.152 0.314574\r
+0.162 40.2069\r
+0.164 148.3954\r
+0.168 598.904\r
+0.172 890.058\r
+0.176 995.096\r
+0.178 1158.031\r
+0.182 1342.306\r
+0.19 1556.716\r
+0.222 1959.8\r
+0.234 2050.53\r
+0.254 2111.01\r
+0.308 2119.9\r
+0.356 2073.29\r
+0.47 2091.07\r
+0.528 1989.543\r
+0.582 1825.825\r
+0.648 1733.526\r
+0.782 1658.07\r
+0.892 1701.725\r
+0.914 1633.231\r
+0.966 1669.558\r
+1.7839 1594.076\r
+1.8239 1551.156\r
+3.1999 1533.43\r
+5.4538 1378.986\r
+6.9577 1170.933\r
+10.9216 424.692\r
+13.5895 106.0499\r
+14.6754 12.60914\r
+16.1354 0.0\r
+++ /dev/null
-; AeroTech N2000W\r
-; Copyright Tripoli Motor Testing 1997 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-N2000W 98 1046 0 7.66707 12.2828 AT\r
- 0.146 2775.075\r
- 0.446 2831.810\r
- 0.746 2834.354\r
- 1.046 2829.564\r
- 1.346 2777.650\r
- 1.646 2688.252\r
- 1.950 2597.973\r
- 2.254 2501.043\r
- 2.554 2415.747\r
- 2.854 2343.624\r
- 3.154 2262.579\r
- 3.454 2178.182\r
- 3.758 2104.164\r
- 4.062 2024.475\r
- 4.362 1935.616\r
- 4.663 1839.781\r
- 4.962 1756.910\r
- 5.262 1351.806\r
- 5.567 954.556\r
- 5.871 681.831\r
- 6.171 475.910\r
- 6.471 361.124\r
- 6.771 194.633\r
- 7.071 44.938\r
- 7.375 6.030\r
- 7.679 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="176.4" Itot="13263.4" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1727.23" burn-time="7.68" cgDiv="10" cgFix="1" cgStep="-1." code="N2000W" delays="1000" dia="98." exitDia="0." initWt="12282.8" len="1046." mDiv="10" mFix="1" mStep="-1." massFrac="62.42" mfg="Aerotech" peakThrust="2834.35" propWt="7667.07" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AeroTech N2000W\r
+Copyright Tripoli Motor Testing 1997 (www.tripoli.org)\r
+provided by ThrustCurve.org (www.thrustcurve.org)\r
+</comments>\r
+<data>\r
+<eng-data cg="523." f="0." m="7667.07" t="0."/>\r
+<eng-data cg="523." f="2775.07" m="7549.97" t="0.146"/>\r
+<eng-data cg="523." f="2831.81" m="7063.8" t="0.446"/>\r
+<eng-data cg="523." f="2834.35" m="6572.49" t="0.746"/>\r
+<eng-data cg="523." f="2829.56" m="6081.38" t="1.046"/>\r
+<eng-data cg="523." f="2777.65" m="5595.18" t="1.346"/>\r
+<eng-data cg="523." f="2688.25" m="5121.24" t="1.646"/>\r
+<eng-data cg="523." f="2597.97" m="4656.76" t="1.95"/>\r
+<eng-data cg="523." f="2501.04" m="4208.74" t="2.254"/>\r
+<eng-data cg="523." f="2415.75" m="3782.41" t="2.554"/>\r
+<eng-data cg="523." f="2343.62" m="3369.73" t="2.854"/>\r
+<eng-data cg="523." f="2262.58" m="2970.33" t="3.154"/>\r
+<eng-data cg="523." f="2178.18" m="2585.27" t="3.454"/>\r
+<eng-data cg="523." f="2104.16" m="2209.01" t="3.758"/>\r
+<eng-data cg="523." f="2024.47" m="1846.24" t="4.062"/>\r
+<eng-data cg="523." f="1935.62" m="1502.87" t="4.362"/>\r
+<eng-data cg="523." f="1839.78" m="1174.41" t="4.663"/>\r
+<eng-data cg="523." f="1756.91" m="863.587" t="4.962"/>\r
+<eng-data cg="523." f="1351.81" m="594.033" t="5.262"/>\r
+<eng-data cg="523." f="954.556" m="390.717" t="5.567"/>\r
+<eng-data cg="523." f="681.831" m="246.935" t="5.871"/>\r
+<eng-data cg="523." f="475.91" m="146.549" t="6.171"/>\r
+<eng-data cg="523." f="361.124" m="73.9703" t="6.471"/>\r
+<eng-data cg="523." f="194.633" m="25.7811" t="6.771"/>\r
+<eng-data cg="523." f="44.938" m="5.00814" t="7.071"/>\r
+<eng-data cg="523." f="6.03" m="0.529827" t="7.375"/>\r
+<eng-data cg="523." f="0." m="0." t="7.679"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+N3300 98 1046 P 7.5120000000000005 12.054 AT\r
+ 0.0070 2069.581\r
+ 0.025 2444.865\r
+ 0.298 2654.583\r
+ 0.852 3068.499\r
+ 1.197 3576.236\r
+ 1.502 3841.143\r
+ 1.719 3929.445\r
+ 2.007 4188.832\r
+ 2.419 4172.276\r
+ 2.753 3885.294\r
+ 3.193 3278.217\r
+ 3.552 2847.744\r
+ 3.786 2665.621\r
+ 3.871 2345.525\r
+ 4.003 866.465\r
+ 4.092 209.718\r
+ 4.18 0.0\r
+++ /dev/null
-; AeroTech N4800T\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-N4800T 98 1194 0 9.7664 14.784 AT\r
- 0.098 4752.717\r
- 0.301 6007.533\r
- 0.506 5594.225\r
- 0.710 5270.361\r
- 0.914 5150.120\r
- 1.119 5108.054\r
- 1.324 5086.206\r
- 1.528 5031.651\r
- 1.731 4941.811\r
- 1.936 4800.400\r
- 2.140 4664.876\r
- 2.344 4527.840\r
- 2.549 4401.003\r
- 2.754 4263.565\r
- 2.958 4120.406\r
- 3.161 3971.136\r
- 3.366 3876.421\r
- 3.570 3916.232\r
- 3.774 3913.510\r
- 3.979 3312.758\r
- 4.184 1649.267\r
- 4.388 523.361\r
- 4.591 327.209\r
- 4.796 251.041\r
- 5.001 128.177\r
- 5.206 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="201.24" Itot="19273.9" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="3702.24" burn-time="5.21" cgDiv="10" cgFix="1" cgStep="-1." code="N4800T" delays="1000" dia="98." exitDia="0." initWt="14784." len="1201." mDiv="10" mFix="1" mStep="-1." massFrac="66.06" mfg="Aerotech" peakThrust="6007.53" propWt="9766.4" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>AeroTech N4800T\r
+provided by ThrustCurve.org (www.thrustcurve.org)\r
+</comments>\r
+<data>\r
+<eng-data cg="600.5" f="0." m="9766.4" t="0."/>\r
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+<eng-data cg="600.5" f="5086.21" m="6330." t="1.324"/>\r
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+<eng-data cg="600.5" f="4263.56" m="2910." t="2.754"/>\r
+<eng-data cg="600.5" f="4120.41" m="2476.67" t="2.958"/>\r
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+<eng-data cg="600.5" f="1649.27" m="212.426" t="4.184"/>\r
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+<eng-data cg="600.5" f="0." m="0." t="5.206"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+I250 54 711 Plugged 0.353 1.855 AHR\r
+ 0.0020 78.6983\r
+ 0.0040 84.8776\r
+ 0.0060 131.6333\r
+ 0.01 285.674\r
+ 0.012 299.107\r
+ 0.016 253.237\r
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+ 0.056 314.198\r
+ 0.116 344.98\r
+ 0.136 317.464\r
+ 0.196 344.409\r
+ 0.21 325.064\r
+ 0.298 341.998\r
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+ 0.33 322.577\r
+ 0.334 345.496\r
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+ 0.7919 294.471\r
+ 1.4618 268.703\r
+ 1.5998 228.345\r
+ 1.8078 92.6199\r
+ 2.3397 16.84115\r
+ 2.7697 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="82.98" Itot="1.221" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1.938" burn-time="0.63" cgDiv="10" cgFix="1" cgStep="-1." code="1/2A2" delays="2,4,6" dia="11." exitDia="0." initWt="4.4" len="57." mDiv="10" mFix="1" mStep="-1." massFrac="34.09" mfg="Apogee" peakThrust="3.97" propWt="1.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <comments>Apogee 1/2A2 RASP.ENG file made from NAR published data\r
+File produced September 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+ <data>\r
+ <eng-data cg="28.5" f="0." m="1.5" t="0."/>\r
+ <eng-data cg="28.5" f="0.19" m="1.49918" t="0.007"/>\r
+ <eng-data cg="28.5" f="1.494" m="1.45986" t="0.045"/>\r
+ <eng-data cg="28.5" f="3.152" m="1.36566" t="0.078"/>\r
+ <eng-data cg="28.5" f="3.805" m="1.32291" t="0.088"/>\r
+ <eng-data cg="28.5" f="3.805" m="1.29954" t="0.093"/>\r
+ <eng-data cg="28.5" f="3.97" m="1.2661" t="0.1"/>\r
+ <eng-data cg="28.5" f="3.696" m="1.24254" t="0.105"/>\r
+ <eng-data cg="28.5" f="3.071" m="1.22176" t="0.11"/>\r
+ <eng-data cg="28.5" f="2.554" m="1.19756" t="0.117"/>\r
+ <eng-data cg="28.5" f="2.582" m="1.17863" t="0.123"/>\r
+ <eng-data cg="28.5" f="2.31" m="1.15158" t="0.132"/>\r
+ <eng-data cg="28.5" f="2.146" m="1.0667" t="0.163"/>\r
+ <eng-data cg="28.5" f="1.984" m="0.972809" t="0.2"/>\r
+ <eng-data cg="28.5" f="1.902" m="0.872527" t="0.242"/>\r
+ <eng-data cg="28.5" f="2.01" m="0.846087" t="0.253"/>\r
+ <eng-data cg="28.5" f="1.929" m="0.792841" t="0.275"/>\r
+ <eng-data cg="28.5" f="1.929" m="0.63402" t="0.342"/>\r
+ <eng-data cg="28.5" f="1.929" m="0.489421" t="0.403"/>\r
+ <eng-data cg="28.5" f="1.848" m="0.473176" t="0.41"/>\r
+ <eng-data cg="28.5" f="1.902" m="0.450135" t="0.42"/>\r
+ <eng-data cg="28.5" f="1.902" m="0.340282" t="0.467"/>\r
+ <eng-data cg="28.5" f="1.929" m="0.196695" t="0.528"/>\r
+ <eng-data cg="28.5" f="1.929" m="0.108988" t="0.565"/>\r
+ <eng-data cg="28.5" f="1.902" m="0.0736794" t="0.58"/>\r
+ <eng-data cg="28.5" f="1.848" m="0.0437259" t="0.593"/>\r
+ <eng-data cg="28.5" f="1.657" m="0.0221902" t="0.603"/>\r
+ <eng-data cg="28.5" f="1.141" m="0.0101559" t="0.61"/>\r
+ <eng-data cg="28.5" f="0.597" m="0.00481652" t="0.615"/>\r
+ <eng-data cg="28.5" f="0.244" m="0.00119937" t="0.622"/>\r
+ <eng-data cg="28.5" f="0." m="-0." t="0.63"/>\r
+ </data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="72.61" Itot="0.57" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2.477" burn-time="0.23" cgDiv="10" cgFix="1" cgStep="-1." code="1/4A2" delays="2,4" dia="11." exitDia="0." initWt="3.6" len="38." mDiv="10" mFix="1" mStep="-1." massFrac="22.22" mfg="Apogee" peakThrust="5.4" propWt="0.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <comments>Apogee 1/4A2 RASP.ENG file made from NAR published data\r
+File produced September 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+ <data>\r
+ <eng-data cg="19." f="0." m="0.8" t="0."/>\r
+ <eng-data cg="19." f="0.162" m="0.799204" t="0.007"/>\r
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+ <eng-data cg="19." f="3.738" m="0.645536" t="0.074"/>\r
+ <eng-data cg="19." f="3.9" m="0.618718" t="0.079"/>\r
+ <eng-data cg="19." f="4.915" m="0.563007" t="0.088"/>\r
+ <eng-data cg="19." f="5.119" m="0.499593" t="0.097"/>\r
+ <eng-data cg="19." f="5.4" m="0.433113" t="0.106"/>\r
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+ <eng-data cg="19." f="3.981" m="0.352445" t="0.118"/>\r
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+ <eng-data cg="19." f="3.453" m="0.279961" t="0.132"/>\r
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+ <eng-data cg="19." f="3.169" m="0.194067" t="0.151"/>\r
+ <eng-data cg="19." f="2.966" m="0.172526" t="0.156"/>\r
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+ <eng-data cg="19." f="2.397" m="0.0787293" t="0.18"/>\r
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+ <eng-data cg="19." f="0.406" m="0.00342121" t="0.218"/>\r
+ <eng-data cg="19." f="0." m="-0." t="0.23"/>\r
+ </data>\r
+ </engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Apogee A2 RASP.ENG file made from NAR published data\r
-;File produced September 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-A2 11 58 0-3-5-7 0.003 0.0067 Apogee \r
-0.014 0.241\r
-0.036 0.895\r
-0.064 2.618\r
-0.1 4.82\r
-0.111 4.133\r
-0.125 2.687\r
-0.139 2.307\r
-0.185 2.031\r
-0.296 1.928\r
-0.481 1.825\r
-0.517 1.722\r
-0.538 1.791\r
-0.649 1.688\r
-0.748 1.757\r
-0.869 1.825\r
-1.04 1.894\r
-1.101 1.894\r
-1.119 1.825\r
-1.144 1.928\r
-1.229 1.859\r
-1.265 1.894\r
-1.283 1.757\r
-1.29 1.412\r
-1.293 0.688\r
-1.3 0.275\r
-1.31 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="84." Itot="2.471" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1.886" burn-time="1.31" cgDiv="10" cgFix="1" cgStep="-1." code="A2" delays="0,3,5,7" dia="11." exitDia="0." initWt="6.7" len="58." mDiv="10" mFix="1" mStep="-1." massFrac="44.78" mfg="Apogee" peakThrust="4.82" propWt="3." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Apogee A2 RASP.ENG file made from NAR published data\r
+File produced September 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+ <eng-data cg="29." f="0." m="3." t="0."/>\r
+ <eng-data cg="29." f="0.241" m="2.99795" t="0.014"/>\r
+ <eng-data cg="29." f="0.895" m="2.98278" t="0.036"/>\r
+ <eng-data cg="29." f="2.618" m="2.92307" t="0.064"/>\r
+ <eng-data cg="29." f="4.82" m="2.76054" t="0.1"/>\r
+ <eng-data cg="29." f="4.133" m="2.70076" t="0.111"/>\r
+ <eng-data cg="29." f="2.687" m="2.6428" t="0.125"/>\r
+ <eng-data cg="29." f="2.307" m="2.60036" t="0.139"/>\r
+ <eng-data cg="29." f="2.031" m="2.47923" t="0.185"/>\r
+ <eng-data cg="29." f="1.928" m="2.21248" t="0.296"/>\r
+ <eng-data cg="29." f="1.825" m="1.79103" t="0.481"/>\r
+ <eng-data cg="29." f="1.722" m="1.71352" t="0.517"/>\r
+ <eng-data cg="29." f="1.791" m="1.66874" t="0.538"/>\r
+ <eng-data cg="29." f="1.688" m="1.43433" t="0.649"/>\r
+ <eng-data cg="29." f="1.757" m="1.22731" t="0.748"/>\r
+ <eng-data cg="29." f="1.825" m="0.96422" t="0.869"/>\r
+ <eng-data cg="29." f="1.894" m="0.578194" t="1.04"/>\r
+ <eng-data cg="29." f="1.894" m="0.437934" t="1.101"/>\r
+ <eng-data cg="29." f="1.825" m="0.397299" t="1.119"/>\r
+ <eng-data cg="29." f="1.928" m="0.340347" t="1.144"/>\r
+ <eng-data cg="29." f="1.859" m="0.144954" t="1.229"/>\r
+ <eng-data cg="29." f="1.894" m="0.0629419" t="1.265"/>\r
+ <eng-data cg="29." f="1.757" m="0.0230505" t="1.283"/>\r
+ <eng-data cg="29." f="1.412" m="0.00958527" t="1.29"/>\r
+ <eng-data cg="29." f="0.688" m="0.00576112" t="1.293"/>\r
+ <eng-data cg="29." f="0.275" m="0.00166927" t="1.3"/>\r
+ <eng-data cg="29." f="0." m="-0." t="1.31"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Apogee B2 RASP.ENG file made from NAR published data\r
-;File produced September 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-B2 11 88 0-3-5-7-9 0.006 0.0106 Apogee \r
-0.057 1.637\r
-0.093 4.091\r
-0.121 5.48\r
-0.143 4.787\r
-0.157 3.478\r
-0.207 2.578\r
-0.328 2.087\r
-0.371 2.087\r
-0.406 1.882\r
-0.641 1.841\r
-0.869 1.841\r
-1.283 1.882\r
-1.361 1.882\r
-1.397 1.718\r
-1.439 1.841\r
-1.532 1.718\r
-1.71 1.841\r
-1.888 1.882\r
-2.095 1.8\r
-2.23 1.8\r
-2.295 1.677\r
-2.423 1.759\r
-2.444 1.637\r
-2.466 0.982\r
-2.494 0.327\r
-2.53 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="81.93" Itot="4.821" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1.905" burn-time="2.53" cgDiv="10" cgFix="1" cgStep="-1." code="B2" delays="0,3,5,7,9" dia="11." exitDia="0." initWt="10.6" len="88." mDiv="10" mFix="1" mStep="-1." massFrac="56.6" mfg="Apogee" peakThrust="5.48" propWt="6." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Apogee B2 RASP.ENG file made from NAR published data\r
+File produced September 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="44." f="0." m="6." t="0."/>\r
+<eng-data cg="44." f="1.637" m="5.94193" t="0.057"/>\r
+<eng-data cg="44." f="4.091" m="5.81361" t="0.093"/>\r
+<eng-data cg="44." f="5.48" m="5.64684" t="0.121"/>\r
+<eng-data cg="44." f="4.787" m="5.50628" t="0.143"/>\r
+<eng-data cg="44." f="3.478" m="5.43428" t="0.157"/>\r
+<eng-data cg="44." f="2.578" m="5.24584" t="0.207"/>\r
+<eng-data cg="44." f="2.087" m="4.89458" t="0.328"/>\r
+<eng-data cg="44." f="2.087" m="4.78289" t="0.371"/>\r
+<eng-data cg="44." f="1.882" m="4.69644" t="0.406"/>\r
+<eng-data cg="44." f="1.841" m="4.15199" t="0.641"/>\r
+<eng-data cg="44." f="1.841" m="3.62957" t="0.869"/>\r
+<eng-data cg="44." f="1.882" m="2.67041" t="1.283"/>\r
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+<eng-data cg="44." f="1.841" m="2.31404" t="1.439"/>\r
+<eng-data cg="44." f="1.718" m="2.10806" t="1.532"/>\r
+<eng-data cg="44." f="1.841" m="1.71383" t="1.71"/>\r
+<eng-data cg="44." f="1.882" m="1.30144" t="1.888"/>\r
+<eng-data cg="44." f="1.8" m="0.827141" t="2.095"/>\r
+<eng-data cg="44." f="1.8" m="0.524704" t="2.23"/>\r
+<eng-data cg="44." f="1.677" m="0.384062" t="2.295"/>\r
+<eng-data cg="44." f="1.759" m="0.11037" t="2.423"/>\r
+<eng-data cg="44." f="1.637" m="0.0659898" t="2.444"/>\r
+<eng-data cg="44." f="0.982" m="0.0301342" t="2.466"/>\r
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+<eng-data cg="44." f="0." m="-0." t="2.53"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Apogee B7 RASP.ENG file made from NAR published data\r
-;File produced September 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-B7 13 50 4-6-8-10 0.0028 0.0091 Apogee \r
-0.007 5.708\r
-0.013 7.211\r
-0.032 6.111\r
-0.045 8.116\r
-0.056 7.717\r
-0.069 9.02\r
-0.078 12.122\r
-0.087 14.76\r
-0.106 13.832\r
-0.117 13.733\r
-0.125 12.636\r
-0.155 12.438\r
-0.168 11.836\r
-0.2 11.243\r
-0.209 11.737\r
-0.219 10.739\r
-0.266 9.846\r
-0.29 9.849\r
-0.299 8.949\r
-0.367 7.456\r
-0.393 7.159\r
-0.429 5.761\r
-0.487 4.567\r
-0.571 2.975\r
-0.607 2.178\r
-0.669 1.084\r
-0.708 0.489\r
-0.74 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="181.04" Itot="4.971" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="6.718" burn-time="0.74" cgDiv="10" cgFix="1" cgStep="-1." code="B7" delays="4,6,8,10" dia="13." exitDia="0." initWt="9.1" len="50." mDiv="10" mFix="1" mStep="-1." massFrac="30.77" mfg="Apogee" peakThrust="14.76" propWt="2.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Apogee B7 RASP.ENG file made from NAR published data\r
+File produced September 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="25." f="0." m="2.8" t="0."/>\r
+<eng-data cg="25." f="5.708" m="2.78875" t="0.007"/>\r
+<eng-data cg="25." f="7.211" m="2.76692" t="0.013"/>\r
+<eng-data cg="25." f="6.111" m="2.69563" t="0.032"/>\r
+<eng-data cg="25." f="8.116" m="2.64354" t="0.045"/>\r
+<eng-data cg="25." f="7.717" m="2.59449" t="0.056"/>\r
+<eng-data cg="25." f="9.02" m="2.53322" t="0.069"/>\r
+<eng-data cg="25." f="12.122" m="2.47963" t="0.078"/>\r
+<eng-data cg="25." f="14.76" m="2.41149" t="0.087"/>\r
+<eng-data cg="25." f="13.832" m="2.2585" t="0.106"/>\r
+<eng-data cg="25." f="13.733" m="2.1731" t="0.117"/>\r
+<eng-data cg="25." f="12.636" m="2.11369" t="0.125"/>\r
+<eng-data cg="25." f="12.438" m="1.90184" t="0.155"/>\r
+<eng-data cg="25." f="11.836" m="1.81297" t="0.168"/>\r
+<eng-data cg="25." f="11.243" m="1.60498" t="0.2"/>\r
+<eng-data cg="25." f="11.737" m="1.54673" t="0.209"/>\r
+<eng-data cg="25." f="10.739" m="1.48343" t="0.219"/>\r
+<eng-data cg="25." f="9.846" m="1.21096" t="0.266"/>\r
+<eng-data cg="25." f="9.849" m="1.07784" t="0.29"/>\r
+<eng-data cg="25." f="8.949" m="1.03019" t="0.299"/>\r
+<eng-data cg="25." f="7.456" m="0.71602" t="0.367"/>\r
+<eng-data cg="25." f="7.159" m="0.609003" t="0.393"/>\r
+<eng-data cg="25." f="5.761" m="0.478011" t="0.429"/>\r
+<eng-data cg="25." f="4.567" m="0.309308" t="0.487"/>\r
+<eng-data cg="25." f="2.975" m="0.130887" t="0.571"/>\r
+<eng-data cg="25." f="2.178" m="0.0786422" t="0.607"/>\r
+<eng-data cg="25." f="1.084" m="0.0216841" t="0.669"/>\r
+<eng-data cg="25." f="0.489" m="0.00440695" t="0.708"/>\r
+<eng-data cg="25." f="0." m="-0." t="0.74"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Apogee C10 RASP.ENG file made from NAR published data\r
-;File produced September 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-C10 18 50 4-7-10 0.0049 0.0176 Apogee \r
-0.01 2.712\r
-0.019 5.842\r
-0.029 17.116\r
-0.037 25.72\r
-0.051 22.535\r
-0.07 20.446\r
-0.106 18.983\r
-0.164 17.085\r
-0.188 17.085\r
-0.2 15.824\r
-0.216 16.036\r
-0.255 15.602\r
-0.293 14.35\r
-0.343 13.503\r
-0.394 12.655\r
-0.41 11.605\r
-0.434 11.605\r
-0.521 9.287\r
-0.631 6.34\r
-0.741 4.021\r
-0.851 2.119\r
-0.911 1.48\r
-0.945 1.264\r
-0.96 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="199.04" Itot="9.564" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="9.963" burn-time="0.96" cgDiv="10" cgFix="1" cgStep="-1." code="C10" delays="4,7,10" dia="18." exitDia="0." initWt="17.6" len="50." mDiv="10" mFix="1" mStep="-1." massFrac="27.84" mfg="Apogee" peakThrust="25.72" propWt="4.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Apogee C10 RASP.ENG file made from NAR published data\r
+File produced September 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="25." f="0." m="4.9" t="0."/>\r
+<eng-data cg="25." f="2.712" m="4.89305" t="0.01"/>\r
+<eng-data cg="25." f="5.842" m="4.87333" t="0.019"/>\r
+<eng-data cg="25." f="17.116" m="4.81452" t="0.029"/>\r
+<eng-data cg="25." f="25.72" m="4.72674" t="0.037"/>\r
+<eng-data cg="25." f="22.535" m="4.55368" t="0.051"/>\r
+<eng-data cg="25." f="20.446" m="4.34449" t="0.07"/>\r
+<eng-data cg="25." f="18.983" m="3.98089" t="0.106"/>\r
+<eng-data cg="25." f="17.085" m="3.44501" t="0.164"/>\r
+<eng-data cg="25." f="17.085" m="3.23494" t="0.188"/>\r
+<eng-data cg="25." f="15.824" m="3.13378" t="0.2"/>\r
+<eng-data cg="25." f="16.036" m="3.0032" t="0.216"/>\r
+<eng-data cg="25." f="15.602" m="2.68712" t="0.255"/>\r
+<eng-data cg="25." f="14.35" m="2.39557" t="0.293"/>\r
+<eng-data cg="25." f="13.503" m="2.03882" t="0.343"/>\r
+<eng-data cg="25." f="12.655" m="1.69709" t="0.394"/>\r
+<eng-data cg="25." f="11.605" m="1.59766" t="0.41"/>\r
+<eng-data cg="25." f="11.605" m="1.45497" t="0.434"/>\r
+<eng-data cg="25." f="9.287" m="0.989366" t="0.521"/>\r
+<eng-data cg="25." f="6.34" m="0.549032" t="0.631"/>\r
+<eng-data cg="25." f="4.021" m="0.257083" t="0.741"/>\r
+<eng-data cg="25." f="2.119" m="0.0840711" t="0.851"/>\r
+<eng-data cg="25." f="1.48" m="0.0287557" t="0.911"/>\r
+<eng-data cg="25." f="1.264" m="0.00485682" t="0.945"/>\r
+<eng-data cg="25." f="0." m="-0." t="0.96"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Apogee C4 RASP.ENG file made from NAR published data\r
-;File produced September 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-C4 18 50 3-5-7 0.0045 0.017 Apogee \r
-0.018 3.23\r
-0.041 6.874\r
-0.147 8.779\r
-0.294 10.683\r
-0.365 11.31\r
-0.388 10.521\r
-0.412 8.779\r
-0.441 7.04\r
-0.465 4.555\r
-0.529 3.479\r
-0.629 2.981\r
-0.653 3.23\r
-0.718 2.816\r
-0.853 2.733\r
-1.065 2.65\r
-1.253 2.567\r
-1.453 2.401\r
-1.694 2.484\r
-1.794 2.484\r
-1.812 2.733\r
-1.841 2.401\r
-1.947 2.401\r
-2.112 2.401\r
-2.235 2.401\r
-2.282 2.236\r
-2.312 1.656\r
-2.329 0.662\r
-2.35 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="202.11" Itot="8.919" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="3.795" burn-time="2.35" cgDiv="10" cgFix="1" cgStep="-1." code="C4" delays="3,5,7" dia="18." exitDia="0." initWt="17." len="50." mDiv="10" mFix="1" mStep="-1." massFrac="26.47" mfg="Apogee" peakThrust="11.31" propWt="4.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Apogee C4 RASP.ENG file made from NAR published data\r
+File produced September 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="25." f="0." m="4.5" t="0."/>\r
+<eng-data cg="25." f="3.23" m="4.48533" t="0.018"/>\r
+<eng-data cg="25." f="6.874" m="4.42671" t="0.041"/>\r
+<eng-data cg="25." f="8.779" m="4.00814" t="0.147"/>\r
+<eng-data cg="25." f="10.683" m="3.28643" t="0.294"/>\r
+<eng-data cg="25." f="11.31" m="2.89252" t="0.365"/>\r
+<eng-data cg="25." f="10.521" m="2.76585" t="0.388"/>\r
+<eng-data cg="25." f="8.779" m="2.649" t="0.412"/>\r
+<eng-data cg="25." f="7.04" m="2.53328" t="0.441"/>\r
+<eng-data cg="25." f="4.555" m="2.46308" t="0.465"/>\r
+<eng-data cg="25." f="3.479" m="2.33337" t="0.529"/>\r
+<eng-data cg="25." f="2.981" m="2.1704" t="0.629"/>\r
+<eng-data cg="25." f="3.23" m="2.1328" t="0.653"/>\r
+<eng-data cg="25." f="2.816" m="2.03366" t="0.718"/>\r
+<eng-data cg="25." f="2.733" m="1.84469" t="0.853"/>\r
+<eng-data cg="25." f="2.65" m="1.5568" t="1.065"/>\r
+<eng-data cg="25." f="2.567" m="1.30938" t="1.253"/>\r
+<eng-data cg="25." f="2.401" m="1.05873" t="1.453"/>\r
+<eng-data cg="25." f="2.484" m="0.761739" t="1.694"/>\r
+<eng-data cg="25." f="2.484" m="0.636413" t="1.794"/>\r
+<eng-data cg="25." f="2.733" m="0.612724" t="1.812"/>\r
+<eng-data cg="25." f="2.401" m="0.575165" t="1.841"/>\r
+<eng-data cg="25." f="2.401" m="0.446759" t="1.947"/>\r
+<eng-data cg="25." f="2.401" m="0.246881" t="2.112"/>\r
+<eng-data cg="25." f="2.401" m="0.0978809" t="2.235"/>\r
+<eng-data cg="25." f="2.236" m="0.0429024" t="2.282"/>\r
+<eng-data cg="25." f="1.656" m="0.0134478" t="2.312"/>\r
+<eng-data cg="25." f="0.662" m="0.003507" t="2.329"/>\r
+<eng-data cg="25." f="0." m="-0." t="2.35"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Apogee C6 RASP.ENG file made from NAR published data\r
-;File produced September 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-C6 13 83 4-7-10 0.007 0.0151 Apogee \r
-0.008 13.958\r
-0.016 21.1\r
-0.022 15.511\r
-0.03 12.831\r
-0.052 14.8\r
-0.081 15.927\r
-0.092 14.658\r
-0.114 16.069\r
-0.125 14.658\r
-0.136 15.369\r
-0.168 14.8\r
-0.214 13.816\r
-0.225 12.973\r
-0.247 13.958\r
-0.252 12.831\r
-0.285 12.547\r
-0.307 12.405\r
-0.317 12.831\r
-0.328 11.562\r
-0.347 11.988\r
-0.393 11.42\r
-0.442 10.719\r
-0.464 11.136\r
-0.488 9.164\r
-0.545 8.459\r
-0.624 7.754\r
-0.716 6.485\r
-0.838 5.075\r
-0.977 3.102\r
-1.096 1.833\r
-1.207 0.986\r
-1.32 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="145.38" Itot="9.98" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="7.56" burn-time="1.32" cgDiv="10" cgFix="1" cgStep="-1." code="C6" delays="4,7,10" dia="13." exitDia="0." initWt="15.1" len="83." mDiv="10" mFix="1" mStep="-1." massFrac="46.36" mfg="Apogee" peakThrust="21.1" propWt="7." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Apogee C6 RASP.ENG file made from NAR published data\r
+File produced September 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="41.5" f="0." m="7." t="0."/>\r
+<eng-data cg="41.5" f="13.958" m="6.96084" t="0.008"/>\r
+<eng-data cg="41.5" f="21.1" m="6.86247" t="0.016"/>\r
+<eng-data cg="41.5" f="15.511" m="6.78543" t="0.022"/>\r
+<eng-data cg="41.5" f="12.831" m="6.70591" t="0.03"/>\r
+<eng-data cg="41.5" f="14.8" m="6.49272" t="0.052"/>\r
+<eng-data cg="41.5" f="15.927" m="6.1802" t="0.081"/>\r
+<eng-data cg="41.5" f="14.658" m="6.0622" t="0.092"/>\r
+<eng-data cg="41.5" f="16.069" m="5.82512" t="0.114"/>\r
+<eng-data cg="41.5" f="14.658" m="5.70658" t="0.125"/>\r
+<eng-data cg="41.5" f="15.369" m="5.59074" t="0.136"/>\r
+<eng-data cg="41.5" f="14.8" m="5.25215" t="0.168"/>\r
+<eng-data cg="41.5" f="13.816" m="4.79049" t="0.214"/>\r
+<eng-data cg="41.5" f="12.973" m="4.68714" t="0.225"/>\r
+<eng-data cg="41.5" f="13.958" m="4.47935" t="0.247"/>\r
+<eng-data cg="41.5" f="12.831" m="4.43237" t="0.252"/>\r
+<eng-data cg="41.5" f="12.547" m="4.13865" t="0.285"/>\r
+<eng-data cg="41.5" f="12.405" m="3.94613" t="0.307"/>\r
+<eng-data cg="41.5" f="12.831" m="3.85762" t="0.317"/>\r
+<eng-data cg="41.5" f="11.562" m="3.76351" t="0.328"/>\r
+<eng-data cg="41.5" f="11.988" m="3.60659" t="0.347"/>\r
+<eng-data cg="41.5" f="11.42" m="3.22894" t="0.393"/>\r
+<eng-data cg="41.5" f="10.719" m="2.84848" t="0.442"/>\r
+<eng-data cg="41.5" f="11.136" m="2.67985" t="0.464"/>\r
+<eng-data cg="41.5" f="9.164" m="2.50898" t="0.488"/>\r
+<eng-data cg="41.5" f="8.459" m="2.15668" t="0.545"/>\r
+<eng-data cg="41.5" f="7.754" m="1.70747" t="0.624"/>\r
+<eng-data cg="41.5" f="6.485" m="1.24804" t="0.716"/>\r
+<eng-data cg="41.5" f="5.075" m="0.753411" t="0.838"/>\r
+<eng-data cg="41.5" f="3.102" m="0.354784" t="0.977"/>\r
+<eng-data cg="41.5" f="1.833" m="0.148819" t="1.096"/>\r
+<eng-data cg="41.5" f="0.986" m="0.0390763" t="1.207"/>\r
+<eng-data cg="41.5" f="0." m="-0." t="1.32"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Apogee D10 RASP.ENG file made from NAR published data\r
-;File produced September 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-D10 18 70 3-5-7 0.0098 0.0259 Apogee \r
-0.011 14.506\r
-0.018 25.13\r
-0.032 20.938\r
-0.079 19.065\r
-0.122 21.139\r
-0.136 19.686\r
-0.169 21.139\r
-0.201 20.728\r
-0.223 21.76\r
-0.233 20.938\r
-0.255 21.97\r
-0.276 20.938\r
-0.352 20.728\r
-0.402 20.107\r
-0.42 20.728\r
-0.459 20.107\r
-0.488 20.517\r
-0.556 18.243\r
-0.671 15.959\r
-0.707 14.717\r
-0.729 15.127\r
-0.779 12.853\r
-0.793 13.474\r
-0.836 11.401\r
-0.904 10.158\r
-0.926 10.569\r
-0.99 8.083\r
-1.026 8.498\r
-1.123 6.011\r
-1.231 2.487\r
-1.342 0.829\r
-1.4 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="195.05" Itot="18.746" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="13.39" burn-time="1.4" cgDiv="10" cgFix="1" cgStep="-1." code="D10" delays="3,5,7" dia="18." exitDia="0." initWt="25.9" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="37.84" mfg="Apogee" peakThrust="25.13" propWt="9.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Apogee D10 RASP.ENG file made from NAR published data\r
+File produced September 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="9.8" t="0."/>\r
+<eng-data cg="35." f="14.506" m="9.75829" t="0.011"/>\r
+<eng-data cg="35." f="25.13" m="9.68577" t="0.018"/>\r
+<eng-data cg="35." f="20.938" m="9.51718" t="0.032"/>\r
+<eng-data cg="35." f="19.065" m="9.02572" t="0.079"/>\r
+<eng-data cg="35." f="21.139" m="8.57383" t="0.122"/>\r
+<eng-data cg="35." f="19.686" m="8.42443" t="0.136"/>\r
+<eng-data cg="35." f="21.139" m="8.07227" t="0.169"/>\r
+<eng-data cg="35." f="20.728" m="7.72207" t="0.201"/>\r
+<eng-data cg="35." f="21.76" m="7.47773" t="0.223"/>\r
+<eng-data cg="35." f="20.938" m="7.36612" t="0.233"/>\r
+<eng-data cg="35." f="21.97" m="7.11937" t="0.255"/>\r
+<eng-data cg="35." f="20.938" m="6.88384" t="0.276"/>\r
+<eng-data cg="35." f="20.728" m="6.0561" t="0.352"/>\r
+<eng-data cg="35." f="20.107" m="5.5224" t="0.402"/>\r
+<eng-data cg="35." f="20.728" m="5.33027" t="0.42"/>\r
+<eng-data cg="35." f="20.107" m="4.91398" t="0.459"/>\r
+<eng-data cg="35." f="20.517" m="4.60603" t="0.488"/>\r
+<eng-data cg="35." f="18.243" m="3.91708" t="0.556"/>\r
+<eng-data cg="35." f="15.959" m="2.88895" t="0.671"/>\r
+<eng-data cg="35." f="14.717" m="2.60029" t="0.707"/>\r
+<eng-data cg="35." f="15.127" m="2.42866" t="0.729"/>\r
+<eng-data cg="35." f="12.853" m="2.06297" t="0.779"/>\r
+<eng-data cg="35." f="13.474" m="1.96663" t="0.793"/>\r
+<eng-data cg="35." f="11.401" m="1.68703" t="0.836"/>\r
+<eng-data cg="35." f="10.158" m="1.30382" t="0.904"/>\r
+<eng-data cg="35." f="10.569" m="1.18463" t="0.926"/>\r
+<eng-data cg="35." f="8.083" m="0.872596" t="0.99"/>\r
+<eng-data cg="35." f="8.498" m="0.716565" t="1.026"/>\r
+<eng-data cg="35." f="6.011" m="0.348685" t="1.123"/>\r
+<eng-data cg="35." f="2.487" m="0.108781" t="1.231"/>\r
+<eng-data cg="35." f="0.829" m="0.0125684" t="1.342"/>\r
+<eng-data cg="35." f="0." m="-0." t="1.4"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Apogee D3 RASP.ENG file made from NAR published data\r
-;File produced September 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-D3 18 77 3-5-7 0.0098 0.0249 Apogee \r
-0.05 6.79\r
-0.168 8.788\r
-0.318 10.46\r
-0.385 10.07\r
-0.402 7.909\r
-0.469 5.432\r
-0.486 3.914\r
-0.687 3.115\r
-1.122 2.876\r
-2.06 2.636\r
-3.349 2.397\r
-4.639 2.156\r
-5.727 1.997\r
-6.163 1.837\r
-6.263 3.994\r
-6.347 2.317\r
-6.364 0.719\r
-6.39 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="191.05" Itot="18.361" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2.873" burn-time="6.39" cgDiv="10" cgFix="1" cgStep="-1." code="D3" delays="3,5,7" dia="18." exitDia="0." initWt="24.9" len="77." mDiv="10" mFix="1" mStep="-1." massFrac="39.36" mfg="Apogee" peakThrust="10.46" propWt="9.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Apogee D3 RASP.ENG file made from NAR published data\r
+File produced September 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="38.5" f="0." m="9.8" t="0."/>\r
+<eng-data cg="38.5" f="6.79" m="9.7094" t="0.05"/>\r
+<eng-data cg="38.5" f="8.788" m="9.21884" t="0.168"/>\r
+<eng-data cg="38.5" f="10.46" m="8.44835" t="0.318"/>\r
+<eng-data cg="38.5" f="10.07" m="8.08127" t="0.385"/>\r
+<eng-data cg="38.5" f="7.909" m="7.9997" t="0.402"/>\r
+<eng-data cg="38.5" f="5.432" m="7.76117" t="0.469"/>\r
+<eng-data cg="38.5" f="3.914" m="7.71877" t="0.486"/>\r
+<eng-data cg="38.5" f="3.115" m="7.34173" t="0.687"/>\r
+<eng-data cg="38.5" f="2.876" m="6.64625" t="1.122"/>\r
+<eng-data cg="38.5" f="2.636" m="5.26648" t="2.06"/>\r
+<eng-data cg="38.5" f="2.397" m="3.53518" t="3.349"/>\r
+<eng-data cg="38.5" f="2.156" m="1.96777" t="4.639"/>\r
+<eng-data cg="38.5" f="1.997" m="0.761945" t="5.727"/>\r
+<eng-data cg="38.5" f="1.837" m="0.315845" t="6.163"/>\r
+<eng-data cg="38.5" f="3.994" m="0.160235" t="6.263"/>\r
+<eng-data cg="38.5" f="2.317" m="0.0187623" t="6.347"/>\r
+<eng-data cg="38.5" f="0.719" m="0.0049888" t="6.364"/>\r
+<eng-data cg="38.5" f="0." m="-0." t="6.39"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech E6 RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-E6 24 70 2-4-6-8-100 0.0215 0.0463 Apogee \r
-0.056 18.59\r
-0.112 20.12\r
-0.168 17.575\r
-0.307 14.38\r
-0.531 10.45\r
-0.894 7.696\r
-1.146 6.244\r
-1.691 5.808\r
-2.836 5.663\r
-3.898 5.517\r
-4.275 5.227\r
-4.415 4.937\r
-5.058 5.082\r
-5.519 5.227\r
-5.603 6.679\r
-5.729 3.921\r
-5.882 2.323\r
-5.966 1.016\r
-6.06 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="183.39" Itot="38.667" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="6.381" burn-time="6.06" cgDiv="10" cgFix="1" cgStep="-1." code="E6" delays="2,4,6,8,100" dia="24." exitDia="0." initWt="46.3" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="46.44" mfg="Apogee" peakThrust="20.12" propWt="21.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech E6 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="21.5" t="0."/>\r
+<eng-data cg="35." f="18.59" m="21.2106" t="0.056"/>\r
+<eng-data cg="35." f="20.12" m="20.6079" t="0.112"/>\r
+<eng-data cg="35." f="17.575" m="20.021" t="0.168"/>\r
+<eng-data cg="35." f="14.38" m="18.7862" t="0.307"/>\r
+<eng-data cg="35." f="10.45" m="17.2399" t="0.531"/>\r
+<eng-data cg="35." f="7.696" m="15.4086" t="0.894"/>\r
+<eng-data cg="35." f="6.244" m="14.432" t="1.146"/>\r
+<eng-data cg="35." f="5.808" m="12.6059" t="1.691"/>\r
+<eng-data cg="35." f="5.663" m="8.95436" t="2.836"/>\r
+<eng-data cg="35." f="5.517" m="5.65345" t="3.898"/>\r
+<eng-data cg="35." f="5.227" m="4.52736" t="4.275"/>\r
+<eng-data cg="35." f="4.937" m="4.13176" t="4.415"/>\r
+<eng-data cg="35." f="5.082" m="2.34073" t="5.058"/>\r
+<eng-data cg="35." f="5.227" m="1.01948" t="5.519"/>\r
+<eng-data cg="35." f="6.679" m="0.741439" t="5.603"/>\r
+<eng-data cg="35." f="3.921" m="0.370124" t="5.729"/>\r
+<eng-data cg="35." f="2.323" m="0.104528" t="5.882"/>\r
+<eng-data cg="35." f="1.016" m="0.0265515" t="5.966"/>\r
+<eng-data cg="35." f="0." m="-0." t="6.06"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Aerotech F10 RASP.ENG file made from NAR published data\r
-;File produced July 4, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-F10 29 93 4-6-8 0.0407 0.0841 Apogee \r
-0.015 28.22\r
-0.077 26.082\r
-0.201 24.934\r
-0.31 22.806\r
-0.464 20.183\r
-0.573 17.886\r
-0.789 16.075\r
-1.068 13.946\r
-1.393 12.63\r
-1.718 11.155\r
-2.166 9.844\r
-2.677 9.515\r
-3.311 9.187\r
-3.683 8.859\r
-3.791 9.679\r
-4.101 9.679\r
-4.658 9.515\r
-5.168 9.023\r
-5.725 9.023\r
-6.112 8.531\r
-6.329 8.859\r
-6.499 7.546\r
-6.685 5.742\r
-6.778 4.921\r
-6.917 2.625\r
-7.025 1.312\r
-7.13 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="191.25" Itot="76.335" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="10.706" burn-time="7.13" cgDiv="10" cgFix="1" cgStep="-1." code="F10" delays="2,4,6,8" dia="29." exitDia="0." initWt="84.1" len="93." mDiv="10" mFix="1" mStep="-1." massFrac="48.39" mfg="Apogee" peakThrust="28.22" propWt="40.7" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F10 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="46.5" f="0." m="40.7" t="0."/>\r
+<eng-data cg="46.5" f="28.22" m="40.5872" t="0.015"/>\r
+<eng-data cg="46.5" f="26.082" m="39.6896" t="0.077"/>\r
+<eng-data cg="46.5" f="24.934" m="38.0032" t="0.201"/>\r
+<eng-data cg="46.5" f="22.806" m="36.6159" t="0.31"/>\r
+<eng-data cg="46.5" f="20.183" m="34.851" t="0.464"/>\r
+<eng-data cg="46.5" f="17.886" m="33.7448" t="0.573"/>\r
+<eng-data cg="46.5" f="16.075" m="31.7892" t="0.789"/>\r
+<eng-data cg="46.5" f="13.946" m="29.5563" t="1.068"/>\r
+<eng-data cg="46.5" f="12.63" m="27.2538" t="1.393"/>\r
+<eng-data cg="46.5" f="11.155" m="25.193" t="1.718"/>\r
+<eng-data cg="46.5" f="9.844" m="22.685" t="2.166"/>\r
+<eng-data cg="46.5" f="9.515" m="20.0478" t="2.677"/>\r
+<eng-data cg="46.5" f="9.187" m="16.8869" t="3.311"/>\r
+<eng-data cg="46.5" f="8.859" m="15.0972" t="3.683"/>\r
+<eng-data cg="46.5" f="9.679" m="14.5635" t="3.791"/>\r
+<eng-data cg="46.5" f="9.679" m="12.9637" t="4.101"/>\r
+<eng-data cg="46.5" f="9.515" m="10.1136" t="4.658"/>\r
+<eng-data cg="46.5" f="9.023" m="7.59314" t="5.168"/>\r
+<eng-data cg="46.5" f="9.023" m="4.91349" t="5.725"/>\r
+<eng-data cg="46.5" f="8.531" m="3.10244" t="6.112"/>\r
+<eng-data cg="46.5" f="8.859" m="2.09644" t="6.329"/>\r
+<eng-data cg="46.5" f="7.546" m="1.35296" t="6.499"/>\r
+<eng-data cg="46.5" f="5.742" m="0.694067" t="6.685"/>\r
+<eng-data cg="46.5" f="4.921" m="0.429701" t="6.778"/>\r
+<eng-data cg="46.5" f="2.625" m="0.150078" t="6.917"/>\r
+<eng-data cg="46.5" f="1.312" m="0.0367253" t="7.025"/>\r
+<eng-data cg="46.5" f="0." m="-0." t="7.13"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="F120-VM" Type="unspecified" dia="29." len="98." initWt="106.2"\r
+propWt="31.4" delays="14,11,9,7,5" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="122.431" peakThrust="143.507" throatDia="0." exitDia="0."\r
+Itot="55.706" burn-time="0.46" massFrac="29.57" Isp="180.91" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Pro29-1G 56F120-VM 14A</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="31.4" cg="49."/>\r
+ <eng-data t="0.013" f="79.242" m="31.1097" cg="49."/>\r
+ <eng-data t="0.017" f="90.427" m="30.9184" cg="49."/>\r
+ <eng-data t="0.04" f="101.422" m="29.6748" cg="49."/>\r
+ <eng-data t="0.125" f="127.583" m="24.1887" cg="49."/>\r
+ <eng-data t="0.179" f="136.114" m="20.1754" cg="49."/>\r
+ <eng-data t="0.222" f="139.905" m="16.8304" cg="49."/>\r
+ <eng-data t="0.289" f="143.507" m="11.4787" cg="49."/>\r
+ <eng-data t="0.354" f="138.578" m="6.31102" cg="49."/>\r
+ <eng-data t="0.394" f="125.498" m="3.33396" cg="49."/>\r
+ <eng-data t="0.406" f="123.602" m="2.49149" cg="49."/>\r
+ <eng-data t="0.416" f="125.118" m="1.7905" cg="49."/>\r
+ <eng-data t="0.423" f="130.047" m="1.2871" cg="49."/>\r
+ <eng-data t="0.431" f="120.569" m="0.722036" cg="49."/>\r
+ <eng-data t="0.447" f="25.592" m="0.0629377" cg="49."/>\r
+ <eng-data t="0.453" f="8.72" m="0.00491524" cg="49."/>\r
+ <eng-data t="0.455" f="0." m="0." cg="49."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; Pro29-1G 55F29-IM 12A\r
+F29-IM 29 98 12-9-7-5-3 0.0376 0.1058 CTI\r
+ 0.0060 5.661\r
+ 0.038 23.312\r
+ 0.05 26.309\r
+ 0.229 30.257\r
+ 0.327 32.208\r
+ 0.485 33.159\r
+ 1.031 31.78\r
+ 1.516 27.07\r
+ 1.688 24.834\r
+ 1.765 20.172\r
+ 1.852 9.467\r
+ 1.963 2.093\r
+ 2.0 0.0\r
--- /dev/null
+F36-BS 29 98 5-7-9-11-14 0.032 0.101 CTI \r
+0.01 12\r
+0.02 25\r
+0.03 41\r
+0.04 42\r
+0.05 42\r
+0.06 40\r
+0.07 34\r
+0.08 34\r
+0.09 35\r
+0.1 36\r
+0.2 40\r
+0.3 42\r
+0.4 43\r
+0.5 43\r
+0.6 43\r
+0.7 43\r
+0.8 42\r
+0.9 41\r
+1 40\r
+1.1 38\r
+1.24 37\r
+1.3 12\r
+1.4 2\r
+1.5 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="F36-SS" Type="unspecified" dia="29." len="98." initWt="104."\r
+propWt="35." delays="2,4,6,8,11" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="39.843" peakThrust="79." throatDia="0." exitDia="0." Itot="41.835"\r
+burn-time="1.05" massFrac="33.65" Isp="121.89" tDiv="10" tStep="-1." tFix="1"\r
+FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="35." cg="49."/>\r
+ <eng-data t="0.01" f="12." m="34.9498" cg="49."/>\r
+ <eng-data t="0.02" f="46." m="34.7072" cg="49."/>\r
+ <eng-data t="0.03" f="75." m="34.201" cg="49."/>\r
+ <eng-data t="0.04" f="79." m="33.5568" cg="49."/>\r
+ <eng-data t="0.06" f="77." m="32.2517" cg="49."/>\r
+ <eng-data t="0.07" f="62." m="31.6703" cg="49."/>\r
+ <eng-data t="0.08" f="32." m="31.277" cg="49."/>\r
+ <eng-data t="0.1" f="35." m="30.7165" cg="49."/>\r
+ <eng-data t="0.2" f="38." m="27.6628" cg="49."/>\r
+ <eng-data t="0.3" f="39." m="24.4419" cg="49."/>\r
+ <eng-data t="0.4" f="41." m="21.0954" cg="49."/>\r
+ <eng-data t="0.5" f="43." m="17.5816" cg="49."/>\r
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+ </data>\r
+ </engine>\r
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--- /dev/null
+F59-WT 29 98 3-5-7-9-12 0.031 0.099 CTI \r
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--- /dev/null
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--- /dev/null
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
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--- /dev/null
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
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--- /dev/null
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--- /dev/null
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+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="G250-VM" Type="unspecified" dia="29." len="142." initWt="141.3"\r
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+ <comments>Pro29-2G 110G250-VM 14A</comments>\r
+ <data>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
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+ <engine-list>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
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--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="G54-RL" Type="unspecified" dia="29." len="187." initWt="198.2"\r
+propWt="96.8" delays="12,9,7,5,3" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="52.725" peakThrust="121.712" throatDia="0." exitDia="0."\r
+Itot="159.544" burn-time="3.03" massFrac="48.84" Isp="168.07" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Pro29-3G 159G54-RL 12A</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="96.8" cg="93.5"/>\r
+ <eng-data t="0.018" f="107.269" m="96.2143" cg="93.5"/>\r
+ <eng-data t="0.031" f="113.588" m="95.3433" cg="93.5"/>\r
+ <eng-data t="0.059" f="103.508" m="93.4992" cg="93.5"/>\r
+ <eng-data t="0.135" f="121.712" m="88.3066" cg="93.5"/>\r
+ <eng-data t="0.22" f="104.561" m="82.4719" cg="93.5"/>\r
+ <eng-data t="0.299" f="95.534" m="77.6765" cg="93.5"/>\r
+ <eng-data t="0.432" f="88.312" m="70.2588" cg="93.5"/>\r
+ <eng-data t="0.959" f="69.657" m="45.0039" cg="93.5"/>\r
+ <eng-data t="1.757" f="43.479" m="17.6154" cg="93.5"/>\r
+ <eng-data t="2.418" f="20.762" m="4.73356" cg="93.5"/>\r
+ <eng-data t="2.851" f="9.478" m="0.761341" cg="93.5"/>\r
+ <eng-data t="3.013" f="5.567" m="0.0219548" cg="93.5"/>\r
+ <eng-data t="3.026" f="0." m="0." cg="93.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+G57-CL 29 142 3-5-7-9-12 0.059 0.146 CTI \r
+0.01 8\r
+0.02 70\r
+0.04 88\r
+0.05 80\r
+0.06 71\r
+0.08 76\r
+0.11 79\r
+0.2 81\r
+0.6 72\r
+1 56\r
+1.5 47\r
+1.6 48\r
+1.7 28\r
+1.8 14\r
+1.9 3\r
+1.93 0\r
+++ /dev/null
-; Cesaroni G60\r
-; Copyright Tripoli Motor Testing 2002 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-G60 38 125 0 0.077056 0.2016 CSR\r
- 0.043 65.216\r
- 0.130 74.906\r
- 0.218 84.596\r
- 0.305 83.963\r
- 0.393 81.982\r
- 0.480 81.956\r
- 0.568 81.138\r
- 0.655 80.530\r
- 0.743 79.923\r
- 0.830 78.867\r
- 0.918 76.675\r
- 1.005 75.118\r
- 1.094 73.732\r
- 1.182 71.315\r
- 1.270 68.781\r
- 1.357 66.853\r
- 1.445 65.111\r
- 1.532 63.526\r
- 1.620 61.229\r
- 1.707 59.249\r
- 1.795 57.110\r
- 1.882 51.671\r
- 1.970 18.562\r
- 2.057 2.667\r
- 2.146 1.470\r
- 2.234 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Cesaroni Technology Inc." code="G60" Type="reloadable" dia="38." len="127."\r
+initWt="201.6" propWt="77.056" delays="12,14" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="62.319" peakThrust="84.596" throatDia="0." exitDia="0." Itot="139.22"\r
+burn-time="2.23" massFrac="38.22" Isp="184.24" tDiv="10" tStep="-1." tFix="1"\r
+FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="77.056" cg="62.5"/>\r
+ <eng-data t="0.043" f="65.216" m="76.2799" cg="62.5"/>\r
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+ <eng-data t="0.218" f="84.596" m="69.0219" cg="62.5"/>\r
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+ <eng-data t="0.393" f="81.982" m="60.9223" cg="62.5"/>\r
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+ <eng-data t="0.83" f="78.867" m="41.3803" cg="62.5"/>\r
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+ <eng-data t="1.182" f="71.315" m="26.7392" cg="62.5"/>\r
+ <eng-data t="1.27" f="68.781" m="23.3274" cg="62.5"/>\r
+ <eng-data t="1.357" f="66.853" m="20.0618" cg="62.5"/>\r
+ <eng-data t="1.445" f="65.111" m="16.848" cg="62.5"/>\r
+ <eng-data t="1.532" f="63.526" m="13.7509" cg="62.5"/>\r
+ <eng-data t="1.62" f="61.229" m="10.7127" cg="62.5"/>\r
+ <eng-data t="1.707" f="59.249" m="7.812" cg="62.5"/>\r
+ <eng-data t="1.795" f="57.11" m="4.97828" cg="62.5"/>\r
+ <eng-data t="1.882" f="51.671" m="2.35922" cg="62.5"/>\r
+ <eng-data t="1.97" f="18.562" m="0.648814" cg="62.5"/>\r
+ <eng-data t="2.057" f="2.667" m="0.137694" cg="62.5"/>\r
+ <eng-data t="2.146" f="1.47" m="0.0357993" cg="62.5"/>\r
+ <eng-data t="2.234" f="0." m="0." cg="62.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
-; Pro38 G69\r
-G69 38 127 5-7-9-12 0.066500 0.2045 Pro38\r
- 0.079 79.935\r
- 0.103 72.367\r
- 0.136 82.989\r
- 0.217 85.910\r
- 0.247 82.193\r
- 0.311 84.317\r
- 0.352 80.201\r
- 0.387 82.856\r
- 0.840 72.499\r
- 0.944 72.234\r
- 0.978 69.047\r
- 1.017 71.835\r
- 1.082 67.852\r
- 1.227 66.657\r
- 1.237 65.329\r
- 1.493 62.010\r
- 1.530 59.354\r
- 1.591 60.151\r
- 1.714 56.167\r
- 1.769 54.574\r
- 1.848 46.607\r
- 1.887 27.884\r
- 1.958 00.000 \r
+; CTI Pro38-1G 117 G69SK - 14A\r
+G69SK 38 126 14-11-9-7-5 0.067 0.198 CTI\r
+ 0.015 49.371\r
+ 0.023 79.41\r
+ 0.035 91.872\r
+ 0.064 82.605\r
+ 0.099 52.407\r
+ 0.166 57.041\r
+ 0.228 59.278\r
+ 0.375 64.231\r
+ 1.297 69.024\r
+ 1.453 68.864\r
+ 1.533 67.746\r
+ 1.589 65.189\r
+ 1.686 58.639\r
+ 1.735 42.821\r
+ 1.781 26.363\r
+ 1.816 13.901\r
+ 1.89 5.432\r
+ 1.954 1.278\r
+ 1.969 0.0\r
-;\r
-133G69 38.0 127.00 3-5-7-9-12 0.08400 0.20510 CTI\r
- 0.06 80.77 \r
- 0.20 84.50 \r
- 0.41 82.74 \r
- 0.59 80.11 \r
- 0.81 76.82 \r
- 1.00 72.87 \r
- 1.20 68.92 \r
- 1.40 64.31 \r
- 1.61 59.48 \r
- 1.82 50.92 \r
- 1.90 21.40 \r
- 1.93 0.00 \r
+; CTI Pro38 G69 Skidmark\r
+G69SK-14A 38 117 5-7-9-11-14 0.0615 0.197 CTI\r
+ 0.025 102.515\r
+ 0.058 97.371\r
+ 0.069 77.862\r
+ 0.088 59.593\r
+ 0.22 72.541\r
+ 0.359 81.054\r
+ 1.036 81.586\r
+ 1.289 75.201\r
+ 1.384 71.831\r
+ 1.488 76.443\r
+ 1.551 64.205\r
+ 1.613 34.053\r
+ 1.696 9.932\r
+ 1.814 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="G69-Classic" Type="reloadable" dia="38."\r
+len="127." initWt="205.1" propWt="84." delays="3,5,7,9,12" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="68.911" peakThrust="84.5" throatDia="0." exitDia="0."\r
+Itot="132.997" burn-time="1.93" massFrac="40.96" Isp="161.45" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Replaced by G46-Classic</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="84." cg="63.5"/>\r
+<eng-data t="0.06" f="80.77" m="82.4696" cg="63.5"/>\r
+<eng-data t="0.2" f="84.5" m="75.1628" cg="63.5"/>\r
+<eng-data t="0.41" f="82.74" m="64.0719" cg="63.5"/>\r
+<eng-data t="0.59" f="80.11" m="54.815" cg="63.5"/>\r
+<eng-data t="0.81" f="76.82" m="43.9122" cg="63.5"/>\r
+<eng-data t="1." f="72.87" m="34.9307" cg="63.5"/>\r
+<eng-data t="1.2" f="68.92" m="25.9753" cg="63.5"/>\r
+<eng-data t="1.4" f="64.31" m="17.5606" cg="63.5"/>\r
+<eng-data t="1.61" f="59.48" m="9.35122" cg="63.5"/>\r
+<eng-data t="1.82" f="50.92" m="2.02981" cg="63.5"/>\r
+<eng-data t="1.9" f="21.4" m="0.202741" cg="63.5"/>\r
+<eng-data t="1.93" f="0." m="0." cg="63.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; Pro38 G69\r
+G69 38 127 5-7-9-12 0.066500 0.2045 Pro38\r
+ 0.079 79.935\r
+ 0.103 72.367\r
+ 0.136 82.989\r
+ 0.217 85.910\r
+ 0.247 82.193\r
+ 0.311 84.317\r
+ 0.352 80.201\r
+ 0.387 82.856\r
+ 0.840 72.499\r
+ 0.944 72.234\r
+ 0.978 69.047\r
+ 1.017 71.835\r
+ 1.082 67.852\r
+ 1.227 66.657\r
+ 1.237 65.329\r
+ 1.493 62.010\r
+ 1.530 59.354\r
+ 1.591 60.151\r
+ 1.714 56.167\r
+ 1.769 54.574\r
+ 1.848 46.607\r
+ 1.887 27.884\r
+ 1.958 00.000 \r
--- /dev/null
+;\r
+133G69 38.0 127.00 3-5-7-9-12 0.08400 0.20510 CTI\r
+ 0.06 80.77 \r
+ 0.20 84.50 \r
+ 0.41 82.74 \r
+ 0.59 80.11 \r
+ 0.81 76.82 \r
+ 1.00 72.87 \r
+ 1.20 68.92 \r
+ 1.40 64.31 \r
+ 1.61 59.48 \r
+ 1.82 50.92 \r
+ 1.90 21.40 \r
+ 1.93 0.00 \r
--- /dev/null
+;CTI Pro38-1G 141 G78BS - 15A\r
+G78BS 38 126 15-12-10-8-6 0.069 0.197 Cesaroni_Technology_Inc. \r
+0.006 104.068\r
+0.018 137.928\r
+0.036 70.707\r
+0.047 62.242\r
+0.084 73.694\r
+0.135 78.176\r
+0.238 84.151\r
+0.438 89.628\r
+0.63 88.135\r
+0.859 87.139\r
+1.283 77.18\r
+1.447 70.707\r
+1.643 67.719\r
+1.713 64.234\r
+1.743 54.275\r
+1.79 18.424\r
+1.818 6.473\r
+1.852 0\r
+++ /dev/null
-;\r
-; Pro38 G79SS\r
-G79SS 38 127 6-8-10-13 0.069000 0.2070 Pro38\r
-0.042 67.279\r
-0.050 72.145\r
-0.065 76.176\r
-0.072 76.176\r
-0.082 74.647\r
-0.094 68.252\r
-0.109 66.167\r
-0.122 65.611\r
-0.433 81.041\r
-0.633 88.130\r
-0.643 87.574\r
-0.684 89.659\r
-0.723 89.798\r
-0.834 92.162\r
-0.939 93.135\r
-1.000 93.969\r
-1.151 91.884\r
-1.160 90.772\r
-1.185 91.189\r
-1.303 86.879\r
-1.499 77.149\r
-1.518 75.064\r
-1.540 66.584\r
-1.587 23.631\r
-1.607 10.982\r
-1.629 4.865\r
-1.631 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="G80-SK" Type="unspecified" dia="29." len="142." initWt="143.2"\r
+propWt="56.4" delays="14,11,9,7,5" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="80.123" peakThrust="108.143" throatDia="0." exitDia="0." Itot="94.385"\r
+burn-time="1.18" massFrac="39.39" Isp="170.65" tDiv="10" tStep="-1." tFix="1"\r
+FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+ <comments>Pro29-3G 93G80-SK 14A</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="56.4" cg="71."/>\r
+ <eng-data t="0.007" f="51.315" m="56.2927" cg="71."/>\r
+ <eng-data t="0.025" f="108.143" m="55.4351" cg="71."/>\r
+ <eng-data t="0.047" f="65.31" m="54.295" cg="71."/>\r
+ <eng-data t="0.122" f="78.032" m="51.083" cg="71."/>\r
+ <eng-data t="0.307" f="89.059" m="41.8473" cg="71."/>\r
+ <eng-data t="0.446" f="93.865" m="34.2504" cg="71."/>\r
+ <eng-data t="0.581" f="95.137" m="26.6271" cg="71."/>\r
+ <eng-data t="0.75" f="91.886" m="17.1837" cg="71."/>\r
+ <eng-data t="0.924" f="84.252" m="8.02684" cg="71."/>\r
+ <eng-data t="0.972" f="83.404" m="5.62245" cg="71."/>\r
+ <eng-data t="1.038" f="88.352" m="2.23555" cg="71."/>\r
+ <eng-data t="1.064" f="67.147" m="1.02761" cg="71."/>\r
+ <eng-data t="1.08" f="40.43" m="0.513348" cg="71."/>\r
+ <eng-data t="1.093" f="21.629" m="0.272306" cg="71."/>\r
+ <eng-data t="1.11" f="9.754" m="0.112906" cg="71."/>\r
+ <eng-data t="1.131" f="2.545" m="0.0357381" cg="71."/>\r
+ <eng-data t="1.178" f="0." m="0." cg="71."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+G83-BS 29 142 5-7-9-11-14 0.058 0.145 CTI \r
+0.01 13\r
+0.02 82\r
+0.03 98\r
+0.04 100\r
+0.05 90\r
+0.06 86\r
+0.12 93\r
+0.2 96\r
+0.3 96\r
+0.7 92\r
+0.9 88\r
+1.07 83\r
+1.1 80\r
+1.2 30\r
+1.3 4\r
+1.33 0\r
--- /dev/null
+G88-SS 29 142 2-4-6-8-11 0.064 0.152 CTI \r
+0.03 7\r
+0.04 60\r
+0.05 90\r
+0.06 113\r
+0.07 116\r
+0.08 113\r
+0.1 86\r
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+0.5 97\r
+0.75 100\r
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+0.84 106\r
+0.9 56\r
+0.93 25\r
+1 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="H100-IM" Type="reloadable" dia="38." len="186." initWt="327."\r
+propWt="154.4" delays="6,8,11,12,15" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="103.403" peakThrust="118." throatDia="0." exitDia="0." Itot="286.427"\r
+burn-time="2.77" massFrac="47.22" Isp="189.17" tDiv="10" tStep="-1." tFix="1"\r
+FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="154.4" cg="93."/>\r
+ <eng-data t="0.016" f="68." m="154.107" cg="93."/>\r
+ <eng-data t="0.056" f="116." m="152.123" cg="93."/>\r
+ <eng-data t="0.09" f="118." m="149.979" cg="93."/>\r
+ <eng-data t="0.14" f="115." m="146.839" cg="93."/>\r
+ <eng-data t="0.5" f="116." m="124.425" cg="93."/>\r
+ <eng-data t="0.6" f="114." m="118.226" cg="93."/>\r
+ <eng-data t="1.25" f="113." m="78.4568" cg="93."/>\r
+ <eng-data t="2.32" f="99." m="17.3172" cg="93."/>\r
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+ <eng-data t="2.55" f="89." m="5.27735" cg="93."/>\r
+ <eng-data t="2.77" f="0." m="0." cg="93."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+H118-CL 29 231 3-5-7-9-12 0.111 0.232 CTI \r
+0.01 7\r
+0.02 144\r
+0.04 183\r
+0.06 182\r
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+1.5 104\r
+1.6 75\r
+1.7 31\r
+1.8 13\r
+1.9 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="H120-RL" Type="reloadable" dia="38."\r
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+auto-calc-cg="1" avgThrust="122.437" peakThrust="147.234" throatDia="0."\r
+exitDia="0." Itot="263.239" burn-time="2.15" massFrac="47.8" Isp="190.38"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="141." cg="63.5"/>\r
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--- /dev/null
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--- /dev/null
+; Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John\r
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--- /dev/null
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--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+ </data>\r
+ </engine>\r
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+</engine-database>\r
--- /dev/null
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+;\r
+;\r
--- /dev/null
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--- /dev/null
+H133-BS 29 187 5-7-9-11-14 0.085 0.19 CTI \r
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--- /dev/null
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--- /dev/null
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--- /dev/null
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+ </data>\r
+ </engine>\r
+</engine-list>\r
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--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+</data>\r
+</engine>\r
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+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Pro29-6G 298H159-GR 15A</comments>\r
+ <data>\r
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+ <eng-data t="1.887" f="0." m="0." cg="160."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+H160-CL 29 320 3-5-7-9-12 0.166 0.319 CTI \r
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--- /dev/null
+<engine-database>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+H163-WT 29 187 5-7-9-11-14 0.086 0.187 CTI \r
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--- /dev/null
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--- /dev/null
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--- /dev/null
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--- /dev/null
+; Pro29-5G 260H194-RL 14A\r
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--- /dev/null
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--- /dev/null
+<engine-database>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; Pro29 6G 311H233-RL 14A\r
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--- /dev/null
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--- /dev/null
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--- /dev/null
+<engine-database>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
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--- /dev/null
+H295-SS 29 320 4-6-8-10-13 0.181 0.342 CTI \r
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--- /dev/null
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+</engine-database>\r
--- /dev/null
+H399-WT 29 320 3-5-7-9-12 0.14 0.294 CTI \r
+0.015 10\r
+0.02 320\r
+0.024 555\r
+0.05 490\r
+0.075 475\r
+0.1 468\r
+0.2 463\r
+0.53 451\r
+0.55 460\r
+0.575 400\r
+0.64 200\r
+0.685 25\r
+0.71 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="H400-Vmax" Type="reloadable" dia="38."\r
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+auto-calc-cg="1" avgThrust="398.559" peakThrust="439.18" throatDia="0."\r
+exitDia="0." Itot="255.078" burn-time="0.64" massFrac="47.67" Isp="192.39"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
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+<eng-data t="0.63" f="117.61" m="0.311687" cg="93."/>\r
+<eng-data t="0.64" f="0." m="0." cg="93."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="H410-VM" Type="unspecified" dia="29." len="187." initWt="182.5"\r
+propWt="84.5" delays="14,11,9,7,5,3" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="402.761" peakThrust="517.452" throatDia="0." exitDia="0."\r
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+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Pro29-3G 168H410-VM 14A</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="84.5" cg="93.5"/>\r
+ <eng-data t="0.004" f="152.778" m="84.3452" cg="93.5"/>\r
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+ <eng-data t="0.414" f="0." m="0." cg="93.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="H565-Vmax" Type="reloadable" dia="38."\r
+len="245." initWt="362.2" propWt="165." delays="5,7,9,11,14" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="560.361" peakThrust="645.28" throatDia="0."\r
+exitDia="0." Itot="319.406" burn-time="0.57" massFrac="48.09" Isp="186.97"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
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+<eng-data t="0.57" f="0." m="0." cg="122.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="H87-IM" Type="reloadable" dia="29." len="187." initWt="205."\r
+propWt="92.7" delays="3,5,7,9,12" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="86.64" peakThrust="139.2" throatDia="0." exitDia="0." Itot="168.082"\r
+burn-time="1.94" massFrac="45.22" Isp="184.89" tDiv="10" tStep="-1." tFix="1"\r
+FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+ <data>\r
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+ <eng-data t="0.018" f="5." m="92.6752" cg="93.5"/>\r
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+ <eng-data t="0.048" f="117." m="91.0586" cg="93.5"/>\r
+ <eng-data t="0.056" f="87." m="90.6086" cg="93.5"/>\r
+ <eng-data t="0.081" f="95." m="89.3539" cg="93.5"/>\r
+ <eng-data t="0.147" f="101." m="85.7867" cg="93.5"/>\r
+ <eng-data t="0.336" f="103." m="75.1546" cg="93.5"/>\r
+ <eng-data t="0.52" f="101." m="64.8037" cg="93.5"/>\r
+ <eng-data t="1.6" f="83." m="10.0051" cg="93.5"/>\r
+ <eng-data t="1.686" f="81." m="6.11576" cg="93.5"/>\r
+ <eng-data t="1.72" f="79." m="4.61564" cg="93.5"/>\r
+ <eng-data t="1.778" f="60." m="2.39248" cg="93.5"/>\r
+ <eng-data t="1.82" f="38." m="1.25746" cg="93.5"/>\r
+ <eng-data t="1.94" f="0." m="0." cg="93.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+H90-CL 29 187 3-5-7-9-12 0.084 0.19 CTI \r
+0.021 10\r
+0.028 154\r
+0.055 155\r
+0.075 108\r
+0.13 120\r
+0.35 115\r
+1.4 83\r
+1.48 84\r
+1.56 73\r
+1.69 22\r
+1.76 8\r
+1.85 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="I120-IM" Type="unspecified" dia="54." len="143." initWt="623.2"\r
+propWt="300." delays="15,14,13,12,11,10,9,8,7,6,5" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="117.259" peakThrust="148.493" throatDia="0."\r
+exitDia="0." Itot="504.215" burn-time="4.3" massFrac="48.14" Isp="171.39"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Pro54-1G 502I120-IM 15A</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="300." cg="71.5"/>\r
+ <eng-data t="0.035" f="13.687" m="299.857" cg="71.5"/>\r
+ <eng-data t="0.047" f="87.183" m="299.497" cg="71.5"/>\r
+ <eng-data t="0.067" f="148.493" m="298.095" cg="71.5"/>\r
+ <eng-data t="0.096" f="129.744" m="295.695" cg="71.5"/>\r
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+ <eng-data t="0.385" f="142.118" m="271.701" cg="71.5"/>\r
+ <eng-data t="0.671" f="141.743" m="247.549" cg="71.5"/>\r
+ <eng-data t="1.032" f="139.681" m="217.325" cg="71.5"/>\r
+ <eng-data t="1.545" f="136.868" m="175.12" cg="71.5"/>\r
+ <eng-data t="2.15" f="127.869" m="127.472" cg="71.5"/>\r
+ <eng-data t="3.757" f="92.433" m="22.1526" cg="71.5"/>\r
+ <eng-data t="4.031" f="89.058" m="7.35878" cg="71.5"/>\r
+ <eng-data t="4.122" f="67.122" m="3.13071" cg="71.5"/>\r
+ <eng-data t="4.216" f="23.436" m="0.59832" cg="71.5"/>\r
+ <eng-data t="4.283" f="5.25" m="0.0265512" cg="71.5"/>\r
+ <eng-data t="4.3" f="0." m="0." cg="71.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="I140-SK" Type="unspecified" dia="54." len="143." initWt="564.29"\r
+propWt="239.2" delays="14,13,12,11,10,9,8,7,6,5,4" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="136.712" peakThrust="160.217" throatDia="0."\r
+exitDia="0." Itot="396.737" burn-time="2.9" massFrac="42.39" Isp="169.13"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Pro54 1G 396 I140-SK 14A</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="239.2" cg="71.5"/>\r
+ <eng-data t="0.008" f="81.304" m="239.004" cg="71.5"/>\r
+ <eng-data t="0.02" f="137.174" m="238.214" cg="71.5"/>\r
+ <eng-data t="0.043" f="157.174" m="236.173" cg="71.5"/>\r
+ <eng-data t="0.065" f="121.087" m="234.327" cg="71.5"/>\r
+ <eng-data t="0.16" f="136.087" m="226.962" cg="71.5"/>\r
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+ <eng-data t="0.54" f="156.304" m="192.975" cg="71.5"/>\r
+ <eng-data t="0.702" f="160.217" m="177.517" cg="71.5"/>\r
+ <eng-data t="0.976" f="156.957" m="151.319" cg="71.5"/>\r
+ <eng-data t="1.298" f="151.304" m="121.396" cg="71.5"/>\r
+ <eng-data t="1.619" f="146.087" m="92.6181" cg="71.5"/>\r
+ <eng-data t="2.057" f="136.304" m="55.3314" cg="71.5"/>\r
+ <eng-data t="2.489" f="121.522" m="21.7547" cg="71.5"/>\r
+ <eng-data t="2.604" f="119.348" m="13.4042" cg="71.5"/>\r
+ <eng-data t="2.671" f="122.174" m="8.52601" cg="71.5"/>\r
+ <eng-data t="2.708" f="111.739" m="5.91695" cg="71.5"/>\r
+ <eng-data t="2.779" f="61.304" m="2.21321" cg="71.5"/>\r
+ <eng-data t="2.84" f="25.217" m="0.622173" cg="71.5"/>\r
+ <eng-data t="2.901" f="8.478" m="0.00255577" cg="71.5"/>\r
+ <eng-data t="2.902" f="0." m="0." cg="71.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; CTI Pro54-1G 465 I150BS 11A\r
+I150BS 54 153 11-10-9-8-7-6-5-4-3-2-1 0.226 0.5700000000000001 CTI\r
+ 0.017 11.039\r
+ 0.039 103.397\r
+ 0.045 164.846\r
+ 0.065 179.932\r
+ 0.09 153.439\r
+ 0.166 162.638\r
+ 0.194 161.902\r
+ 0.303 169.261\r
+ 0.483 171.837\r
+ 0.666 173.309\r
+ 0.834 171.469\r
+ 1.275 168.525\r
+ 1.725 156.015\r
+ 2.559 128.05\r
+ 2.77 122.53\r
+ 2.899 118.851\r
+ 2.978 119.219\r
+ 3.003 99.349\r
+ 3.034 82.791\r
+ 3.087 66.233\r
+ 3.16 19.502\r
+ 3.208 0.0\r
; Cesaroni I170\r
-; Copyright Tripoli Motor Testing 2002 (www.tripoli.org)\r
+; converted from TMT test stand data 2002 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
I170 38 242 0 0.209216 0.404992 CSR\r
0.044 133.251\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="I170-Classic" Type="reloadable" dia="38."\r
+len="245." initWt="392." propWt="187.5" delays="14,9,7,5,3" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="140.258" peakThrust="206.689" throatDia="0."\r
+exitDia="0." Itot="378.696" burn-time="2.7" massFrac="51.79" Isp="190.23"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
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+<eng-data t="0.4" f="179.455" m="170.369" cg="122.5"/>\r
+<eng-data t="0.5" f="180.744" m="160.715" cg="122.5"/>\r
+<eng-data t="0.6" f="182.603" m="150.976" cg="122.5"/>\r
+<eng-data t="0.7" f="186.51" m="141.083" cg="122.5"/>\r
+<eng-data t="0.8" f="186.585" m="131.083" cg="122.5"/>\r
+<eng-data t="0.9" f="187.951" m="121.045" cg="122.5"/>\r
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+<eng-data t="1.1" f="189.506" m="100.804" cg="122.5"/>\r
+<eng-data t="1.2" f="184.917" m="90.7685" cg="122.5"/>\r
+<eng-data t="1.3" f="184.537" m="80.8663" cg="122.5"/>\r
+<eng-data t="1.4" f="184.993" m="70.9619" cg="122.5"/>\r
+<eng-data t="1.5" f="183.21" m="61.0932" cg="122.5"/>\r
+<eng-data t="1.6" f="182.072" m="51.3027" cg="122.5"/>\r
+<eng-data t="1.7" f="182.565" m="41.5295" cg="122.5"/>\r
+<eng-data t="1.8" f="177.975" m="31.8662" cg="122.5"/>\r
+<eng-data t="1.9" f="173.84" m="22.4366" cg="122.5"/>\r
+<eng-data t="2." f="156.657" m="13.5785" cg="122.5"/>\r
+<eng-data t="2.1" f="98.736" m="6.73332" cg="122.5"/>\r
+<eng-data t="2.2" f="42.976" m="2.93509" cg="122.5"/>\r
+<eng-data t="2.3" f="19.08" m="1.27183" cg="122.5"/>\r
+<eng-data t="2.4" f="8.8" m="0.524578" cg="122.5"/>\r
+<eng-data t="2.5" f="2.883" m="0.211445" cg="122.5"/>\r
+<eng-data t="2.6" f="2.503" m="0.0670866" cg="122.5"/>\r
+<eng-data t="2.7" f="0." m="0." cg="122.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; CTI Pro38-3G 338 I180 Skidmark 14A\r
+I180SK 38 243 5-7-9-11-14 0.2 0.394 CTI\r
+ 0.0030 130.431\r
+ 0.028 173.405\r
+ 0.062 156.065\r
+ 0.197 180.945\r
+ 0.644 206.578\r
+ 0.962 214.872\r
+ 1.336 205.07\r
+ 1.482 199.039\r
+ 1.585 196.777\r
+ 1.638 171.143\r
+ 1.7 91.226\r
+ 1.795 24.88\r
+ 1.962 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="I195-RL" Type="reloadable" dia="38."\r
+len="245." initWt="417." propWt="226." delays="7,9,11,13,16" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="195.675" peakThrust="235.422" throatDia="0."\r
+exitDia="0." Itot="395.264" burn-time="2.02" massFrac="54.2" Isp="178.34"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="226." cg="122.5"/>\r
+<eng-data t="0." f="10.17" m="226." cg="122.5"/>\r
+<eng-data t="0.01" f="67.545" m="225.778" cg="122.5"/>\r
+<eng-data t="0.02" f="179.678" m="225.071" cg="122.5"/>\r
+<eng-data t="0.03" f="203.433" m="223.976" cg="122.5"/>\r
+<eng-data t="0.04" f="206.127" m="222.805" cg="122.5"/>\r
+<eng-data t="0.05" f="192.2" m="221.666" cg="122.5"/>\r
+<eng-data t="0.06" f="195.73" m="220.557" cg="122.5"/>\r
+<eng-data t="0.07" f="177.667" m="219.49" cg="122.5"/>\r
+<eng-data t="0.08" f="181.689" m="218.462" cg="122.5"/>\r
+<eng-data t="0.09" f="186.85" m="217.409" cg="122.5"/>\r
+<eng-data t="0.1" f="195.73" m="216.315" cg="122.5"/>\r
+<eng-data t="0.2" f="226.58" m="204.242" cg="122.5"/>\r
+<eng-data t="0.3" f="235.422" m="191.034" cg="122.5"/>\r
+<eng-data t="0.4" f="231.02" m="177.699" cg="122.5"/>\r
+<eng-data t="0.5" f="231.703" m="164.47" cg="122.5"/>\r
+<eng-data t="0.6" f="226.011" m="151.385" cg="122.5"/>\r
+<eng-data t="0.7" f="222.596" m="138.56" cg="122.5"/>\r
+<eng-data t="0.8" f="223.696" m="125.801" cg="122.5"/>\r
+<eng-data t="0.9" f="210.567" m="113.386" cg="122.5"/>\r
+<eng-data t="1." f="208.48" m="101.406" cg="122.5"/>\r
+<eng-data t="1.1" f="205.482" m="89.5719" cg="122.5"/>\r
+<eng-data t="1.2" f="204.002" m="77.8654" cg="122.5"/>\r
+<eng-data t="1.3" f="196.602" m="66.4128" cg="122.5"/>\r
+<eng-data t="1.4" f="191.517" m="55.317" cg="122.5"/>\r
+<eng-data t="1.5" f="188.633" m="44.4491" cg="122.5"/>\r
+<eng-data t="1.6" f="183.511" m="33.8101" cg="122.5"/>\r
+<eng-data t="1.7" f="186.357" m="23.2362" cg="122.5"/>\r
+<eng-data t="1.8" f="181.727" m="12.7132" cg="122.5"/>\r
+<eng-data t="1.9" f="113.726" m="4.26665" cg="122.5"/>\r
+<eng-data t="2." f="29.598" m="0.169232" cg="122.5"/>\r
+<eng-data t="2.02" f="0." m="0." cg="122.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+I204-IM 29 320 4-6-8-10-13 0.194 0.349 CTI \r
+0.01 100\r
+0.012 395\r
+0.03 310\r
+0.3 286\r
+0.5 270\r
+0.7 251\r
+1 228\r
+1.1 215\r
+1.2 165\r
+1.3 125\r
+1.4 95\r
+1.5 52\r
+1.6 36\r
+1.72 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="I205-Classic" Type="reloadable" dia="38."\r
+len="245." initWt="402.2" propWt="206.1" delays="5,7,9,11,14" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="203.999" peakThrust="235.8" throatDia="0."\r
+exitDia="0." Itot="383.518" burn-time="1.88" massFrac="51.24" Isp="189.75"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Replaced by I170 Classic</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="206.1" cg="122.5"/>\r
+<eng-data t="0.1" f="181.5" m="201.223" cg="122.5"/>\r
+<eng-data t="0.13" f="213.3" m="198.041" cg="122.5"/>\r
+<eng-data t="0.2" f="210.1" m="190.077" cg="122.5"/>\r
+<eng-data t="0.4" f="226.61" m="166.609" cg="122.5"/>\r
+<eng-data t="0.6" f="235.8" m="141.759" cg="122.5"/>\r
+<eng-data t="0.8" f="234." m="116.512" cg="122.5"/>\r
+<eng-data t="1." f="232.8" m="91.4266" cg="122.5"/>\r
+<eng-data t="1.2" f="227.7" m="66.6797" cg="122.5"/>\r
+<eng-data t="1.4" f="216.8" m="42.7925" cg="122.5"/>\r
+<eng-data t="1.6" f="197.21" m="20.5439" cg="122.5"/>\r
+<eng-data t="1.74" f="183.13" m="6.2364" cg="122.5"/>\r
+<eng-data t="1.8" f="87.3" m="1.87658" cg="122.5"/>\r
+<eng-data t="1.88" f="0." m="0." cg="122.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="I212-SS" Type="reloadable" dia="38."\r
+len="245." initWt="475." propWt="248.1" delays="5,7,9,11,14" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="213.061" peakThrust="255.15" throatDia="0."\r
+exitDia="0." Itot="364.334" burn-time="1.71" massFrac="52.23" Isp="149.75"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="248.1" cg="122.5"/>\r
+<eng-data t="0.04" f="189.66" m="245.517" cg="122.5"/>\r
+<eng-data t="0.2" f="207.11" m="223.902" cg="122.5"/>\r
+<eng-data t="0.4" f="222.41" m="194.653" cg="122.5"/>\r
+<eng-data t="0.6" f="236.62" m="163.395" cg="122.5"/>\r
+<eng-data t="0.8" f="249.6" m="130.284" cg="122.5"/>\r
+<eng-data t="0.95" f="255.15" m="104.506" cg="122.5"/>\r
+<eng-data t="1.01" f="250.22" m="94.1814" cg="122.5"/>\r
+<eng-data t="1.21" f="233.54" m="61.2388" cg="122.5"/>\r
+<eng-data t="1.4" f="208.99" m="32.6107" cg="122.5"/>\r
+<eng-data t="1.55" f="183.99" m="12.5402" cg="122.5"/>\r
+<eng-data t="1.6" f="168.08" m="6.54649" cg="122.5"/>\r
+<eng-data t="1.63" f="134.62" m="3.45455" cg="122.5"/>\r
+<eng-data t="1.69" f="25.86" m="0.176098" cg="122.5"/>\r
+<eng-data t="1.71" f="0." m="0." cg="122.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="I216-CL(I)" Type="reloadable" dia="38." len="367." initWt="601."\r
+propWt="312.5" delays="5,7,9,11,14" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="205.198" peakThrust="345." throatDia="0." exitDia="0." Itot="636.114"\r
+burn-time="3.1" massFrac="52." Isp="207.57" tDiv="10" tStep="-1." tFix="1"\r
+FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+ <comments>This motor is a standard Pro38-5G with a different nozzle to keep total impulse in 'I' range</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="312.5" cg="183.5"/>\r
+ <eng-data t="0.017" f="35." m="312.354" cg="183.5"/>\r
+ <eng-data t="0.03" f="300." m="311.284" cg="183.5"/>\r
+ <eng-data t="0.035" f="345." m="310.492" cg="183.5"/>\r
+ <eng-data t="0.05" f="325." m="308.023" cg="183.5"/>\r
+ <eng-data t="0.07" f="275." m="305.076" cg="183.5"/>\r
+ <eng-data t="0.14" f="292." m="295.327" cg="183.5"/>\r
+ <eng-data t="0.26" f="296." m="277.995" cg="183.5"/>\r
+ <eng-data t="0.8" f="280." m="201.593" cg="183.5"/>\r
+ <eng-data t="1.1" f="280.4" m="160.298" cg="183.5"/>\r
+ <eng-data t="1.62" f="255." m="91.9118" cg="183.5"/>\r
+ <eng-data t="1.8" f="226." m="70.645" cg="183.5"/>\r
+ <eng-data t="2.105" f="210." m="37.9809" cg="183.5"/>\r
+ <eng-data t="2.2" f="195." m="28.5302" cg="183.5"/>\r
+ <eng-data t="2.45" f="80." m="11.643" cg="183.5"/>\r
+ <eng-data t="2.75" f="36." m="3.09496" cg="183.5"/>\r
+ <eng-data t="3.1" f="0." m="0." cg="183.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; CTI Pro54-1G 491 I218WT - 14A\r
+I218WT 54 153 14-13-12-11-10-9-8-7-6-5-4 0.23 0.58 CTI\r
+ 0.01 12.222\r
+ 0.022 129.788\r
+ 0.047 215.926\r
+ 0.072 250.846\r
+ 0.079 208.36\r
+ 0.11 233.968\r
+ 0.188 249.1\r
+ 0.436 263.651\r
+ 0.783 258.994\r
+ 1.195 235.714\r
+ 1.614 201.375\r
+ 1.834 191.481\r
+ 1.964 183.915\r
+ 2.074 178.095\r
+ 2.143 179.841\r
+ 2.172 87.884\r
+ 2.188 50.053\r
+ 2.217 18.624\r
+ 2.252 0.0\r
--- /dev/null
+; CTI Pro38-4G 434 I223 Skidmark 14A\r
+I223SK 38 302 5-7-9-11-14 0.266 0.494 CTI\r
+ 0.016 199.183\r
+ 0.024 260.157\r
+ 0.07 207.313\r
+ 0.148 227.637\r
+ 0.425 244.71\r
+ 0.721 254.466\r
+ 1.015 256.905\r
+ 1.3 248.775\r
+ 1.459 240.645\r
+ 1.615 234.954\r
+ 1.712 195.931\r
+ 1.782 119.51\r
+ 1.9 24.39\r
+ 1.984 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="I224-CL" Type="unspecified" dia="29." len="365." initWt="370."\r
+propWt="196.7" delays="15,12,10,8,6" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="223.658" peakThrust="433.079" throatDia="0." exitDia="0."\r
+Itot="380.218" burn-time="1.7" massFrac="53.16" Isp="197.11" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Pro29-6GXL 381I224-CL 15A</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="196.7" cg="182.5"/>\r
+ <eng-data t="0.008" f="357.455" m="195.96" cg="182.5"/>\r
+ <eng-data t="0.02" f="433.079" m="193.506" cg="182.5"/>\r
+ <eng-data t="0.111" f="343.833" m="175.219" cg="182.5"/>\r
+ <eng-data t="0.229" f="318.938" m="154.989" cg="182.5"/>\r
+ <eng-data t="0.479" f="295.922" m="115.228" cg="182.5"/>\r
+ <eng-data t="0.836" f="277.133" m="62.3099" cg="182.5"/>\r
+ <eng-data t="1.022" f="269.618" m="36.0045" cg="182.5"/>\r
+ <eng-data t="1.097" f="233.919" m="26.2359" cg="182.5"/>\r
+ <eng-data t="1.233" f="117.899" m="13.8594" cg="182.5"/>\r
+ <eng-data t="1.294" f="93.004" m="10.5316" cg="182.5"/>\r
+ <eng-data t="1.39" f="62.003" m="6.68245" cg="182.5"/>\r
+ <eng-data t="1.667" f="26.774" m="0.321495" cg="182.5"/>\r
+ <eng-data t="1.692" f="17.38" m="0.0359651" cg="182.5"/>\r
+ <eng-data t="1.7" f="0." m="0." cg="182.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+I236BS 38 245 17-14-12-10-8 0.20400000000000001 0.4 Cesaroni\r
+ 0.028 290.772\r
+ 0.042 313.594\r
+ 0.049 267.95\r
+ 0.053 253.58\r
+ 0.072 245.973\r
+ 0.095 256.961\r
+ 0.127 262.033\r
+ 0.153 266.259\r
+ 0.243 268.795\r
+ 0.338 269.64\r
+ 0.454 270.486\r
+ 0.633 266.259\r
+ 0.753 262.878\r
+ 0.89 256.116\r
+ 1.01 251.89\r
+ 1.119 247.663\r
+ 1.277 236.675\r
+ 1.353 231.603\r
+ 1.453 227.377\r
+ 1.525 225.686\r
+ 1.555 195.257\r
+ 1.581 158.91\r
+ 1.618 119.183\r
+ 1.685 89.598\r
+ 1.729 56.633\r
+ 1.743 36.347\r
+ 1.766 21.977\r
+ 1.81 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Cesaroni" code="I236-Blue Streak" Type="reloadable" dia="38." len="245."\r
+initWt="400." propWt="204." delays="17,14,12,10,8" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="229.006" peakThrust="313.594" throatDia="0."\r
+exitDia="0." Itot="414.501" burn-time="1.81" massFrac="51." Isp="207.19"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="204." cg="122.5"/>\r
+ <eng-data t="0.028" f="290.772" m="201.997" cg="122.5"/>\r
+ <eng-data t="0.042" f="313.594" m="199.914" cg="122.5"/>\r
+ <eng-data t="0.049" f="267.95" m="198.913" cg="122.5"/>\r
+ <eng-data t="0.053" f="253.58" m="198.399" cg="122.5"/>\r
+ <eng-data t="0.072" f="245.973" m="196.064" cg="122.5"/>\r
+ <eng-data t="0.095" f="256.961" m="193.217" cg="122.5"/>\r
+ <eng-data t="0.127" f="262.033" m="189.13" cg="122.5"/>\r
+ <eng-data t="0.153" f="266.259" m="185.75" cg="122.5"/>\r
+ <eng-data t="0.243" f="268.795" m="173.9" cg="122.5"/>\r
+ <eng-data t="0.338" f="269.64" m="161.313" cg="122.5"/>\r
+ <eng-data t="0.454" f="270.486" m="145.895" cg="122.5"/>\r
+ <eng-data t="0.633" f="266.259" m="122.253" cg="122.5"/>\r
+ <eng-data t="0.753" f="262.878" m="106.627" cg="122.5"/>\r
+ <eng-data t="0.89" f="256.116" m="89.1307" cg="122.5"/>\r
+ <eng-data t="1.01" f="251.89" m="74.1295" cg="122.5"/>\r
+ <eng-data t="1.119" f="247.663" m="60.7302" cg="122.5"/>\r
+ <eng-data t="1.277" f="236.675" m="41.899" cg="122.5"/>\r
+ <eng-data t="1.353" f="231.603" m="33.1412" cg="122.5"/>\r
+ <eng-data t="1.453" f="227.377" m="21.8467" cg="122.5"/>\r
+ <eng-data t="1.525" f="225.686" m="13.8195" cg="122.5"/>\r
+ <eng-data t="1.555" f="195.257" m="10.7119" cg="122.5"/>\r
+ <eng-data t="1.581" f="158.91" m="8.44594" cg="122.5"/>\r
+ <eng-data t="1.618" f="119.183" m="5.91393" cg="122.5"/>\r
+ <eng-data t="1.685" f="89.598" m="2.4717" cg="122.5"/>\r
+ <eng-data t="1.729" f="56.633" m="0.888384" cg="122.5"/>\r
+ <eng-data t="1.743" f="36.347" m="0.568058" cg="122.5"/>\r
+ <eng-data t="1.766" f="21.977" m="0.237955" cg="122.5"/>\r
+ <eng-data t="1.81" f="0." m="0." cg="122.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Cesaroni I240\r
-; Copyright Tripoli Motor Testing 2002 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I240 38 302 0 0.274624 0.503552 CSR\r
- 0.043 265.317\r
- 0.131 320.903\r
- 0.221 314.148\r
- 0.310 312.413\r
- 0.399 313.564\r
- 0.488 314.335\r
- 0.577 321.117\r
- 0.667 325.923\r
- 0.755 327.040\r
- 0.844 326.831\r
- 0.933 324.348\r
- 1.023 321.063\r
- 1.111 317.446\r
- 1.200 308.301\r
- 1.290 300.612\r
- 1.379 293.536\r
- 1.468 283.358\r
- 1.556 273.832\r
- 1.646 259.708\r
- 1.735 190.662\r
- 1.824 124.130\r
- 1.912 60.875\r
- 2.002 26.967\r
- 2.092 7.636\r
- 2.181 2.296\r
- 2.271 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="I240" Type="reloadable" dia="38."\r
+len="302." initWt="503.552" propWt="274.624" delays="15" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="241.841" peakThrust="327.04" throatDia="0."\r
+exitDia="0." Itot="549.221" burn-time="2.27" massFrac="54.54" Isp="203.93"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="274.624" cg="151."/>\r
+<eng-data t="0.043" f="265.317" m="271.772" cg="151."/>\r
+<eng-data t="0.131" f="320.903" m="258.874" cg="151."/>\r
+<eng-data t="0.221" f="314.148" m="244.585" cg="151."/>\r
+<eng-data t="0.31" f="312.413" m="230.643" cg="151."/>\r
+<eng-data t="0.399" f="313.564" m="216.715" cg="151."/>\r
+<eng-data t="0.488" f="314.335" m="202.743" cg="151."/>\r
+<eng-data t="0.577" f="321.117" m="188.604" cg="151."/>\r
+<eng-data t="0.667" f="325.923" m="174.045" cg="151."/>\r
+<eng-data t="0.755" f="327.04" m="159.679" cg="151."/>\r
+<eng-data t="0.844" f="326.831" m="145.129" cg="151."/>\r
+<eng-data t="0.933" f="324.348" m="130.64" cg="151."/>\r
+<eng-data t="1.023" f="321.063" m="116.117" cg="151."/>\r
+<eng-data t="1.111" f="317.446" m="102.07" cg="151."/>\r
+<eng-data t="1.2" f="308.301" m="88.146" cg="151."/>\r
+<eng-data t="1.29" f="300.612" m="74.4448" cg="151."/>\r
+<eng-data t="1.379" f="293.536" m="61.2243" cg="151."/>\r
+<eng-data t="1.468" f="283.358" m="48.3878" cg="151."/>\r
+<eng-data t="1.556" f="273.832" m="36.129" cg="151."/>\r
+<eng-data t="1.646" f="259.708" m="24.1238" cg="151."/>\r
+<eng-data t="1.735" f="190.662" m="14.1026" cg="151."/>\r
+<eng-data t="1.824" f="124.13" m="7.09812" cg="151."/>\r
+<eng-data t="1.912" f="60.875" m="3.02781" cg="151."/>\r
+<eng-data t="2.002" f="26.967" m="1.05127" cg="151."/>\r
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+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="I255-16A" Type="reloadable" dia="38." len="303." initWt="516."\r
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+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Pro-38 Red Lightning 4 Grain reload</comments>\r
+ <data>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="I285-Classic" Type="reloadable" dia="38."\r
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+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; CTI Pro38-5G 543 I297 Skidmark 15A\r
+I297SM 38 360 6-8-10-12-15 0.329 0.591 CTI\r
+ 0.013 340.903\r
+ 0.036 375.121\r
+ 0.069 354.844\r
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+ 1.681 69.701\r
+ 1.74 40.554\r
+ 1.846 12.673\r
+ 1.943 0.0\r
--- /dev/null
+I303BS 38 303 16-13-11-9-7 0.27 0.5 Cesaroni\r
+ 0.035 415.763\r
+ 0.053 402.352\r
+ 0.054 329.705\r
+ 0.072 324.117\r
+ 0.109 348.705\r
+ 0.18 353.175\r
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+ 1.475 292.823\r
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+ 1.609 149.764\r
+ 1.639 108.411\r
+ 1.757 50.294\r
+ 1.827 22.353\r
+ 1.887 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-I350SS 38.0 367.00 7-9-11-13-16 0.41350 0.78200 CTI\r
- 0.05 399.74 \r
- 0.13 390.06 \r
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- 0.40 388.13 \r
- 0.60 388.13 \r
- 0.80 388.13 \r
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- 1.44 350.38 \r
- 1.52 320.37 \r
- 1.60 164.79 \r
- 1.68 36.77 \r
- 1.71 0.00 \r
--- /dev/null
+<engine-database>\r
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+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-I360 38 367 15 0.3346 0.5963 Cesaroni\r
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--- /dev/null
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--- /dev/null
+I445-VM 54 143 6-7-8-9-10-11-12-13-14-15-16 0.242 0.575 CTI \r
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--- /dev/null
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+ <eng-data t="0.0393701" f="506.89" m="238.036" cg="151.5"/>\r
+ <eng-data t="0.0682415" f="518.959" m="231.25" cg="151.5"/>\r
+ <eng-data t="0.0944882" f="518.959" m="225.009" cg="151.5"/>\r
+ <eng-data t="0.131234" f="520.683" m="216.256" cg="151.5"/>\r
+ <eng-data t="0.178478" f="524.132" m="204.946" cg="151.5"/>\r
+ <eng-data t="0.217848" f="525.856" m="195.475" cg="151.5"/>\r
+ <eng-data t="0.267717" f="525.856" m="183.458" cg="151.5"/>\r
+ <eng-data t="0.299213" f="527.58" m="175.856" cg="151.5"/>\r
+ <eng-data t="0.346457" f="522.407" m="164.49" cg="151.5"/>\r
+ <eng-data t="0.388451" f="520.683" m="154.453" cg="151.5"/>\r
+ <eng-data t="0.422572" f="522.407" m="146.299" cg="151.5"/>\r
+ <eng-data t="0.459318" f="525.856" m="137.473" cg="151.5"/>\r
+ <eng-data t="0.509186" f="522.407" m="125.496" cg="151.5"/>\r
+ <eng-data t="0.553806" f="517.235" m="114.867" cg="151.5"/>\r
+ <eng-data t="0.585302" f="515.511" m="107.414" cg="151.5"/>\r
+ <eng-data t="0.637795" f="515.511" m="95.0137" cg="151.5"/>\r
+ <eng-data t="0.687664" f="508.615" m="83.312" cg="151.5"/>\r
+ <eng-data t="0.729659" f="505.166" m="73.5575" cg="151.5"/>\r
+ <eng-data t="0.771654" f="508.615" m="63.803" cg="151.5"/>\r
+ <eng-data t="0.824147" f="503.442" m="51.6306" cg="151.5"/>\r
+ <eng-data t="0.860892" f="496.546" m="43.2115" cg="151.5"/>\r
+ <eng-data t="0.900262" f="494.822" m="34.2688" cg="151.5"/>\r
+ <eng-data t="0.926509" f="491.373" m="28.3381" cg="151.5"/>\r
+ <eng-data t="0.973753" f="482.753" m="17.7936" cg="151.5"/>\r
+ <eng-data t="0.997375" f="415.512" m="12.9319" cg="151.5"/>\r
+ <eng-data t="1.00525" f="374.133" m="11.5072" cg="151.5"/>\r
+ <eng-data t="1.02362" f="337.927" m="8.50976" cg="151.5"/>\r
+ <eng-data t="1.04987" f="282.755" m="4.77716" cg="151.5"/>\r
+ <eng-data t="1.06562" f="231.032" m="2.92331" cg="151.5"/>\r
+ <eng-data t="1.07612" f="181.032" m="1.9321" cg="151.5"/>\r
+ <eng-data t="1.08661" f="134.481" m="1.17313" cg="151.5"/>\r
+ <eng-data t="1.09974" f="86.2059" m="0.509562" cg="151.5"/>\r
+ <eng-data t="1.11024" f="32.7582" m="0.223396" cg="151.5"/>\r
+ <eng-data t="1.14" f="0." m="0." cg="151.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="I566-Vmax" Type="reloadable" dia="38."\r
+len="245." initWt="384.2" propWt="197.8" delays="6,8,10,12,15" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="569.516" peakThrust="628.65" throatDia="0."\r
+exitDia="0." Itot="370.185" burn-time="0.65" massFrac="51.48" Isp="190.84"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="197.8" cg="122.5"/>\r
+<eng-data t="0.01" f="396.82" m="196.74" cg="122.5"/>\r
+<eng-data t="0.02" f="462.72" m="194.443" cg="122.5"/>\r
+<eng-data t="0.04" f="473.24" m="189.442" cg="122.5"/>\r
+<eng-data t="0.07" f="512.07" m="181.545" cg="122.5"/>\r
+<eng-data t="0.1" f="537.85" m="173.13" cg="122.5"/>\r
+<eng-data t="0.15" f="572.85" m="158.293" cg="122.5"/>\r
+<eng-data t="0.2" f="587.73" m="142.79" cg="122.5"/>\r
+<eng-data t="0.25" f="600.41" m="126.919" cg="122.5"/>\r
+<eng-data t="0.3" f="609.75" m="110.753" cg="122.5"/>\r
+<eng-data t="0.4" f="611.42" m="78.1279" cg="122.5"/>\r
+<eng-data t="0.5" f="602.61" m="45.6935" cg="122.5"/>\r
+<eng-data t="0.6" f="600.26" m="13.5572" cg="122.5"/>\r
+<eng-data t="0.61" f="607.55" m="10.3303" cg="122.5"/>\r
+<eng-data t="0.62" f="628.65" m="7.02766" cg="122.5"/>\r
+<eng-data t="0.63" f="612.18" m="3.71261" cg="122.5"/>\r
+<eng-data t="0.64" f="388.73" m="1.03854" cg="122.5"/>\r
+<eng-data t="0.65" f="0." m="0." cg="122.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="I800-Vmax" Type="reloadable" dia="38."\r
+len="303." initWt="457." propWt="232.5" delays="6,8,10,12,16" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="798.968" peakThrust="888.69" throatDia="0."\r
+exitDia="0." Itot="415.464" burn-time="0.52" massFrac="50.88" Isp="182.22"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="232.5" cg="151.5"/>\r
+<eng-data t="0.01" f="276.1" m="231.727" cg="151.5"/>\r
+<eng-data t="0.02" f="680.47" m="229.051" cg="151.5"/>\r
+<eng-data t="0.05" f="741.02" m="217.119" cg="151.5"/>\r
+<eng-data t="0.1" f="791.43" m="195.679" cg="151.5"/>\r
+<eng-data t="0.2" f="830.85" m="150.286" cg="151.5"/>\r
+<eng-data t="0.3" f="851.45" m="103.214" cg="151.5"/>\r
+<eng-data t="0.4" f="853.81" m="55.4997" cg="151.5"/>\r
+<eng-data t="0.5" f="888.69" m="6.74312" cg="151.5"/>\r
+<eng-data t="0.51" f="760.61" m="2.12825" cg="151.5"/>\r
+<eng-data t="0.52" f="0." m="0." cg="151.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="J1055-Vmax" Type="unspecified" dia="54." len="236."\r
+initWt="772." propWt="379." delays="17,15,13,10,7" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="1007.5" peakThrust="1117.9" throatDia="0."\r
+exitDia="0." Itot="738.499" burn-time="0.733" massFrac="49.0933" Isp="198.696"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="379." cg="118."/>\r
+ <eng-data t="0.01" f="412.26" m="377.942" cg="118."/>\r
+ <eng-data t="0.02" f="896.44" m="374.584" cg="118."/>\r
+ <eng-data t="0.03" f="1056.8" m="369.572" cg="118."/>\r
+ <eng-data t="0.04" f="1100.26" m="364.037" cg="118."/>\r
+ <eng-data t="0.05" f="1065.65" m="358.479" cg="118."/>\r
+ <eng-data t="0.06" f="1041.03" m="353.073" cg="118."/>\r
+ <eng-data t="0.07" f="1011.42" m="347.807" cg="118."/>\r
+ <eng-data t="0.08" f="998.73" m="342.649" cg="118."/>\r
+ <eng-data t="0.09" f="1027.96" m="337.448" cg="118."/>\r
+ <eng-data t="0.1" f="1051.03" m="332.113" cg="118."/>\r
+ <eng-data t="0.15" f="1086.41" m="304.69" cg="118."/>\r
+ <eng-data t="0.2" f="1101.8" m="276.615" cg="118."/>\r
+ <eng-data t="0.3" f="1117.9" m="219.657" cg="118."/>\r
+ <eng-data t="0.4" f="1110.26" m="162.482" cg="118."/>\r
+ <eng-data t="0.5" f="1103.72" m="105.671" cg="118."/>\r
+ <eng-data t="0.6" f="1112.95" m="48.7909" cg="118."/>\r
+ <eng-data t="0.67" f="1045.65" m="10.0178" cg="118."/>\r
+ <eng-data t="0.68" f="748.38" m="5.41432" cg="118."/>\r
+ <eng-data t="0.69" f="382.65" m="2.51208" cg="118."/>\r
+ <eng-data t="0.7" f="172.67" m="1.08712" cg="118."/>\r
+ <eng-data t="0.71" f="80.38" m="0.437786" cg="118."/>\r
+ <eng-data t="0.72" f="39.23" m="0.130864" cg="118."/>\r
+ <eng-data t="0.733" f="0." m="0." cg="118."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="J1365ST" Type="reloadable" dia="54."\r
+len="326." initWt="1200." propWt="444." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="1355.49" peakThrust="1576.58" throatDia="0."\r
+exitDia="0." Itot="931.222" burn-time="0.69" massFrac="29.6" Isp="213.87"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve from the AMW web site and CAR/NAR/TRA certified\r
+rocket motor list dated 9/28/08. The total weight was estimated based on\r
+similar motors such as the J325TT, J395RR, and the J401BB</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="444." cg="163."/>\r
+<eng-data t="0.007" f="1576.58" m="441.369" cg="163."/>\r
+<eng-data t="0.011" f="1083.9" m="438.832" cg="163."/>\r
+<eng-data t="0.014" f="1402.03" m="437.054" cg="163."/>\r
+<eng-data t="0.019" f="1083.9" m="434.091" cg="163."/>\r
+<eng-data t="0.023" f="1402.03" m="431.72" cg="163."/>\r
+<eng-data t="0.027" f="1196.52" m="429.242" cg="163."/>\r
+<eng-data t="0.03" f="1266.9" m="427.481" cg="163."/>\r
+<eng-data t="0.049" f="1311.94" m="415.8" cg="163."/>\r
+<eng-data t="0.078" f="1379.51" m="397.192" cg="163."/>\r
+<eng-data t="0.124" f="1447.08" m="366.195" cg="163."/>\r
+<eng-data t="0.164" f="1483.68" m="338.248" cg="163."/>\r
+<eng-data t="0.219" f="1514.65" m="298.935" cg="163."/>\r
+<eng-data t="0.267" f="1523.09" m="264.174" cg="163."/>\r
+<eng-data t="0.311" f="1531.54" m="232.132" cg="163."/>\r
+<eng-data t="0.361" f="1525.91" m="195.688" cg="163."/>\r
+<eng-data t="0.391" f="1506.2" m="174.003" cg="163."/>\r
+<eng-data t="0.455" f="1447.08" m="128.943" cg="163."/>\r
+<eng-data t="0.489" f="1418.93" m="105.713" cg="163."/>\r
+<eng-data t="0.526" f="1393.59" m="80.9048" cg="163."/>\r
+<eng-data t="0.564" f="1371.07" m="55.8597" cg="163."/>\r
+<eng-data t="0.595" f="1354.17" m="35.7194" cg="163."/>\r
+<eng-data t="0.612" f="1342.91" m="24.7888" cg="163."/>\r
+<eng-data t="0.62" f="1334.47" m="19.6826" cg="163."/>\r
+<eng-data t="0.624" f="1300.68" m="17.1697" cg="163."/>\r
+<eng-data t="0.633" f="1185.25" m="11.836" cg="163."/>\r
+<eng-data t="0.643" f="881.198" m="6.90964" cg="163."/>\r
+<eng-data t="0.649" f="661.602" m="4.70285" cg="163."/>\r
+<eng-data t="0.655" f="458.899" m="3.10011" cg="163."/>\r
+<eng-data t="0.663" f="289.979" m="1.67187" cg="163."/>\r
+<eng-data t="0.676" f="135.136" m="0.354375" cg="163."/>\r
+<eng-data t="0.687" f="0." m="0." cg="163."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="J1520-Vmax" Type="unspecified" dia="54." len="329."\r
+initWt="1026." propWt="544." delays="17,15,13,10,7" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="1453.13" peakThrust="1661.73" throatDia="0."\r
+exitDia="0." Itot="1070.95" burn-time="0.737" massFrac="53.0214" Isp="200.748"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="544." cg="164.5"/>\r
+ <eng-data t="0.01" f="216.51" m="543.45" cg="164.5"/>\r
+ <eng-data t="0.02" f="1199.48" m="539.854" cg="164.5"/>\r
+ <eng-data t="0.03" f="1182.56" m="533.804" cg="164.5"/>\r
+ <eng-data t="0.04" f="1265.24" m="527.587" cg="164.5"/>\r
+ <eng-data t="0.05" f="1373.3" m="520.886" cg="164.5"/>\r
+ <eng-data t="0.06" f="1505.21" m="513.575" cg="164.5"/>\r
+ <eng-data t="0.07" f="1549.44" m="505.817" cg="164.5"/>\r
+ <eng-data t="0.08" f="1515.59" m="498.032" cg="164.5"/>\r
+ <eng-data t="0.09" f="1498.67" m="490.377" cg="164.5"/>\r
+ <eng-data t="0.1" f="1484.06" m="482.801" cg="164.5"/>\r
+ <eng-data t="0.15" f="1569.82" m="444.02" cg="164.5"/>\r
+ <eng-data t="0.2" f="1590.97" m="403.881" cg="164.5"/>\r
+ <eng-data t="0.3" f="1618.27" m="322.373" cg="164.5"/>\r
+ <eng-data t="0.4" f="1624.04" m="240.025" cg="164.5"/>\r
+ <eng-data t="0.5" f="1661.73" m="156.574" cg="164.5"/>\r
+ <eng-data t="0.6" f="1599.05" m="73.7566" cg="164.5"/>\r
+ <eng-data t="0.67" f="1466.75" m="19.2512" cg="164.5"/>\r
+ <eng-data t="0.68" f="1293.31" m="12.2412" cg="164.5"/>\r
+ <eng-data t="0.69" f="920.66" m="6.61821" cg="164.5"/>\r
+ <eng-data t="0.7" f="537.63" m="2.91446" cg="164.5"/>\r
+ <eng-data t="0.71" f="213.05" m="1.00789" cg="164.5"/>\r
+ <eng-data t="0.72" f="68.07" m="0.293902" cg="164.5"/>\r
+ <eng-data t="0.737" f="0." m="0." cg="164.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J210 54.0 236.00 6-16 0.08270 0.84200 CTI\r
- 0.04 335.00 \r
- 0.16 270.92 \r
- 0.41 269.30 \r
- 0.80 268.49 \r
- 1.18 256.32 \r
- 1.62 236.85 \r
- 2.03 214.14 \r
- 2.38 193.86 \r
- 2.79 174.39 \r
- 3.20 163.85 \r
- 3.60 157.36 \r
- 3.75 135.46 \r
- 3.86 85.17 \r
- 3.99 0.00 \r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="J210" Type="reloadable" dia="54."\r
+len="236." initWt="842." propWt="439." delays="6,16" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="205.674" peakThrust="315.824" throatDia="0."\r
+exitDia="0." Itot="843.262" burn-time="4.1" massFrac="52.14" Isp="195.87"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="439." cg="118."/>\r
+<eng-data t="0.05" f="315.824" m="434.89" cg="118."/>\r
+<eng-data t="0.08" f="229.083" m="430.634" cg="118."/>\r
+<eng-data t="0.15" f="257.107" m="421.776" cg="118."/>\r
+<eng-data t="0.2" f="263.779" m="414.996" cg="118."/>\r
+<eng-data t="0.25" f="274.01" m="407.997" cg="118."/>\r
+<eng-data t="0.3" f="272.676" m="400.882" cg="118."/>\r
+<eng-data t="0.35" f="276.679" m="393.732" cg="118."/>\r
+<eng-data t="0.4" f="276.679" m="386.53" cg="118."/>\r
+<eng-data t="0.5" f="278.014" m="372.092" cg="118."/>\r
+<eng-data t="0.7" f="273.566" m="343.377" cg="118."/>\r
+<eng-data t="0.8" f="275.345" m="329.088" cg="118."/>\r
+<eng-data t="1.6" f="240.204" m="221.731" cg="118."/>\r
+<eng-data t="2.8" f="179.263" m="90.7071" cg="118."/>\r
+<eng-data t="3." f="173.481" m="72.3433" cg="118."/>\r
+<eng-data t="3.05" f="169.032" m="67.8856" cg="118."/>\r
+<eng-data t="3.4" f="164.584" m="37.4916" cg="118."/>\r
+<eng-data t="3.5" f="164.584" m="28.9234" cg="118."/>\r
+<eng-data t="3.6" f="160.136" m="20.471" cg="118."/>\r
+<eng-data t="3.7" f="146.791" m="12.4818" cg="118."/>\r
+<eng-data t="3.8" f="104.088" m="5.95142" cg="118."/>\r
+<eng-data t="3.9" f="48.93" m="1.96838" cg="118."/>\r
+<eng-data t="4." f="13.345" m="0.347368" cg="118."/>\r
+<eng-data t="4.1" f="0." m="0." cg="118."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="J240-RL" Type="unspecified" dia="54." len="236." initWt="875."\r
+propWt="469." delays="6,9,11,13,16" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="241.624" peakThrust="292.642" throatDia="0." exitDia="0."\r
+Itot="808.959" burn-time="3.348" massFrac="53.6" Isp="175.887" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="469." cg="118."/>\r
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+ <eng-data t="0.02" f="24.087" m="468.854" cg="118."/>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; CTI Pro54-2G 683 I250 Skidmark 15A\r
+J250SK 54 237 6-8-10-12-15 0.406 0.8300000000000001 CTI\r
+ 0.031 191.478\r
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+ 2.825 6.263\r
+ 2.965 0.0\r
+++ /dev/null
-;\r
-;\r
-J280SS 54.0 236.00 6-16 0.51200 0.95400 CTI\r
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- 2.44 178.24 \r
- 2.49 42.80 \r
- 2.54 0.00 \r
--- /dev/null
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+++ /dev/null
-;\r
-;\r
-J285 38.0 367.00 6-8-10-12-15 0.31250 0.59500 CTI\r
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- 2.25 11.02 \r
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--- /dev/null
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+</engine>\r
+</engine-list>\r
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--- /dev/null
+; CTI Pro54-2G 838 J293BS 13A\r
+J293BS 54 237 13-12-11-10-9-8-7-6-5-4-3 0.41600000000000004 0.84 CTI\r
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+++ /dev/null
-;\r
-;\r
-J295 54.0 329.00 6-16 0.59400 1.11900 CTI\r
- 0.04 450.52 \r
- 0.28 428.70 \r
- 0.54 423.25 \r
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- 3.00 243.26 \r
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- 3.67 126.54 \r
- 3.82 64.36 \r
- 4.00 0.00 \r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+</data>\r
+</engine>\r
+</engine-list>\r
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+++ /dev/null
-; Cesaroni J300\r
-; Copyright Tripoli Motor Testing 2002 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J300 38 360 0 0.340032 0.606592 CSR\r
- 0.043 357.026\r
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- 1.917 71.413\r
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--- /dev/null
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+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Cesaroni Technology Inc." code="J325TT" Type="reloadable" dia="54."\r
+len="326." initWt="1230." propWt="537." delays="1000" auto-calc-mass="1"\r
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+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John\r
+Coker. Data from CAR web site, thrust curve from AMW web site.\r
+</comments>\r
+ <data>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="J3354-15A" Type="reloadable" dia="38." len="367." initWt="627."\r
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+ <comments>Pro-38 Red Lightning 5G.</comments>\r
+ <data>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+J357BS 38 367 17-14-12-10-8 0.337 0.601 Cesaroni\r
+ 0.019 514.383\r
+ 0.042 502.824\r
+ 0.054 446.473\r
+ 0.073 434.914\r
+ 0.122 433.469\r
+ 0.258 430.579\r
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+ 1.236 381.453\r
+ 1.386 372.784\r
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+ 1.487 345.33\r
+ 1.515 317.877\r
+ 1.552 268.751\r
+ 1.615 196.506\r
+ 1.655 134.375\r
+ 1.721 49.127\r
+ 1.758 26.008\r
+ 1.824 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Cesaroni" code="J357-Blue Streak" Type="reloadable" dia="38." len="367."\r
+initWt="601." propWt="337." delays="17,14,12,10,8" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="360.248" peakThrust="514.383" throatDia="0."\r
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+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
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+ <eng-data t="1.824" f="0." m="0." cg="183.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
-; Cesaroni J360\r
-; Copyright Tripoli Motor Testing 2002 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J360 38 419 0 0.409024 0.709184 CSR\r
- 0.041 618.905\r
- 0.124 616.584\r
- 0.207 563.785\r
- 0.291 557.730\r
- 0.374 558.409\r
- 0.457 562.088\r
- 0.541 561.267\r
- 0.624 563.219\r
- 0.708 565.328\r
- 0.793 566.558\r
- 0.876 549.383\r
- 0.959 529.633\r
- 1.043 511.099\r
- 1.126 483.285\r
- 1.209 445.397\r
- 1.293 421.658\r
- 1.377 378.330\r
- 1.461 261.647\r
- 1.545 197.445\r
- 1.628 146.570\r
- 1.711 101.807\r
- 1.795 78.039\r
- 1.878 47.847\r
- 1.961 31.861\r
- 2.046 9.220\r
- 2.130 0.000\r
+; CTI Pro54-3G 1016 J3360 Skidmark 15A\r
+J360SM 54 321 6-8-10-12-15 0.606 1.104 CTI\r
+ 0.017 560.653\r
+ 0.058 287.423\r
+ 0.167 328.23\r
+ 0.358 363.715\r
+ 0.538 374.36\r
+ 0.85 397.425\r
+ 1.163 400.973\r
+ 1.458 400.973\r
+ 1.733 395.651\r
+ 1.983 381.457\r
+ 2.271 356.618\r
+ 2.496 340.65\r
+ 2.592 351.295\r
+ 2.646 289.198\r
+ 2.679 172.099\r
+ 2.725 86.937\r
+ 2.804 19.516\r
+ 2.904 5.323\r
+ 2.975 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="J360" Type="reloadable" dia="38."\r
+len="419." initWt="709.184" propWt="409.024" delays="15" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="383.009" peakThrust="618.905" throatDia="0."\r
+exitDia="0." Itot="815.809" burn-time="2.13" massFrac="57.68" Isp="203.39"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
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+<eng-data t="2.13" f="0." m="0." cg="209.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="J380-SS" Type="reloadable" dia="54."\r
+len="320." initWt="1293.3" propWt="769." delays="6,16" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="382.191" peakThrust="434.6" throatDia="0."\r
+exitDia="0." Itot="1043.38" burn-time="2.73" massFrac="59.46" Isp="138.36"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="769." cg="160."/>\r
+<eng-data t="0.05" f="368.48" m="762.211" cg="160."/>\r
+<eng-data t="0.3" f="348.31" m="696.174" cg="160."/>\r
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+<eng-data t="2.73" f="0." m="0." cg="160."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; CTI Pro38-6G 660 G381SK - 15A\r
+J381SK 38 419 15-12-10-8-6 0.396 0.6880000000000001 CTI\r
+ 0.048 505.029\r
+ 0.111 473.244\r
+ 0.294 461.471\r
+ 0.968 436.75\r
+ 1.353 392.015\r
+ 1.385 366.116\r
+ 1.556 137.735\r
+ 1.662 47.089\r
+ 1.706 22.367\r
+ 1.874 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Cesaroni Technology Inc." code="J395RR" Type="reloadable" dia="54."\r
+len="326." initWt="1268." propWt="573." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="391.129" peakThrust="467.063" throatDia="0."\r
+exitDia="0." Itot="1079.52" burn-time="2.76" massFrac="45.19" Isp="192.11"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John\r
+Coker. Data from CAR web site, thrust curve from AMW web site.\r
+</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="573." cg="163."/>\r
+ <eng-data t="0.032" f="336.088" m="570.146" cg="163."/>\r
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+++ /dev/null
-;\r
-;\r
-J400SS 38.0 421.00 7-9-11-13-16 0.48960 0.70200 CTI\r
- 0.05 451.79 \r
- 0.20 461.14 \r
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--- /dev/null
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--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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--- /dev/null
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--- /dev/null
+J420-CL 38 500 6-8-10-12-15 0.522 0.874 CTI \r
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--- /dev/null
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--- /dev/null
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--- /dev/null
+J440-BB 54 326 0 0.536 1.229 AMW/ProX \r
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--- /dev/null
+; CTI Pro54-3G 1261 J449BS 15A\r
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--- /dev/null
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--- /dev/null
+<engine-database>\r
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--- /dev/null
+J530-IM 38 500 6-8-10-12-15 0.625 0.977 CTI \r
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--- /dev/null
+; CTI Pro38-6GXL 896 J580SS - 17A\r
+J580SS 38 510 17-14-12-10-8 0.6880000000000001 1.044 CTI\r
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+ 1.613 0.0\r
--- /dev/null
+; CTI Pro38-6GXL 999 J600RL - 16A\r
+J600RL 38 510 16-13-11-9-7 0.551 0.906 CTI\r
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--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+</comments>\r
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--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; Blue Baboon\r
+K1130-BB 54 728 0 1.359 2.574 AMW/ProX \r
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--- /dev/null
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+<eng-data t="0.3" f="1319.85" m="796.689" cg="244."/>\r
+<eng-data t="0.4" f="1331.39" m="732.008" cg="244."/>\r
+<eng-data t="0.5" f="1325.23" m="667.196" cg="244."/>\r
+<eng-data t="0.7" f="1323.31" m="537.966" cg="244."/>\r
+<eng-data t="0.8" f="1304.08" m="473.866" cg="244."/>\r
+<eng-data t="0.9" f="1280.62" m="410.809" cg="244."/>\r
+<eng-data t="1." f="1249.86" m="349.074" cg="244."/>\r
+<eng-data t="1.1" f="1217.94" m="288.868" cg="244."/>\r
+<eng-data t="1.2" f="1199.29" m="229.896" cg="244."/>\r
+<eng-data t="1.3" f="1158.77" m="172.367" cg="244."/>\r
+<eng-data t="1.4" f="1112.56" m="116.955" cg="244."/>\r
+<eng-data t="1.5" f="1099.87" m="62.9789" cg="244."/>\r
+<eng-data t="1.55" f="941.81" m="38.0739" cg="244."/>\r
+<eng-data t="1.6" f="726.07" m="17.7286" cg="244."/>\r
+<eng-data t="1.62" f="559.17" m="11.4575" cg="244."/>\r
+<eng-data t="1.64" f="399.95" m="6.7777" cg="244."/>\r
+<eng-data t="1.66" f="317.66" m="3.27626" cg="244."/>\r
+<eng-data t="1.67" f="247.28" m="1.898" cg="244."/>\r
+<eng-data t="1.68" f="198.05" m="0.811551" cg="244."/>\r
+<eng-data t="1.69" f="67.3" m="0.164189" cg="244."/>\r
+<eng-data t="1.7" f="0." m="0." cg="244."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+K1250-WW 54 491 0 0.925 1.815 AMW/ProX \r
+0.01 600\r
+0.02 1400\r
+0.03 1610\r
+0.05 1360\r
+0.07 1410\r
+0.1 1440\r
+0.15 1470\r
+0.2 1480\r
+0.4 1480\r
+0.8 1395\r
+1.28 1185\r
+1.36 985\r
+1.4 680\r
+1.45 570\r
+1.5 210\r
+1.6 60\r
+1.7 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="K1440WT" Type="reloadable" dia="54."\r
+len="572." initWt="1892.6" propWt="1162.4" delays="7,17" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="1426.68" peakThrust="2168.21" throatDia="0."\r
+exitDia="0." Itot="2368.29" burn-time="1.66" massFrac="61.42" Isp="207.76"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="1162.4" cg="286."/>\r
+<eng-data t="0.01" f="1061.8" m="1159.79" cg="286."/>\r
+<eng-data t="0.01" f="2168.21" m="1159.79" cg="286."/>\r
+<eng-data t="0.02" f="2036.3" m="1149.48" cg="286."/>\r
+<eng-data t="0.07" f="1691.73" m="1103.73" cg="286."/>\r
+<eng-data t="0.1" f="1805.18" m="1077.99" cg="286."/>\r
+<eng-data t="0.2" f="1747.49" m="990.8" cg="286."/>\r
+<eng-data t="0.3" f="1721.72" m="905.663" cg="286."/>\r
+<eng-data t="0.4" f="1712.49" m="821.384" cg="286."/>\r
+<eng-data t="0.5" f="1709.03" m="737.417" cg="286."/>\r
+<eng-data t="0.6" f="1682.11" m="654.195" cg="286."/>\r
+<eng-data t="0.7" f="1678.65" m="571.719" cg="286."/>\r
+<eng-data t="0.8" f="1638.27" m="490.318" cg="286."/>\r
+<eng-data t="0.9" f="1601.35" m="410.815" cg="286."/>\r
+<eng-data t="1.01" f="1539.56" m="326.026" cg="286."/>\r
+<eng-data t="1.11" f="1462.58" m="252.351" cg="286."/>\r
+<eng-data t="1.21" f="1398.43" m="182.139" cg="286."/>\r
+<eng-data t="1.3" f="1111.41" m="126.704" cg="286."/>\r
+<eng-data t="1.4" f="1039.5" m="73.919" cg="286."/>\r
+<eng-data t="1.45" f="922.2" m="49.848" cg="286."/>\r
+<eng-data t="1.5" f="701.07" m="29.9297" cg="286."/>\r
+<eng-data t="1.55" f="556.47" m="14.4991" cg="286."/>\r
+<eng-data t="1.6" f="272.66" m="4.32529" cg="286."/>\r
+<eng-data t="1.65" f="66.53" m="0.163271" cg="286."/>\r
+<eng-data t="1.66" f="0." m="0." cg="286."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="K160-CL" Type="unspecified" dia="54." len="404." initWt="1472."\r
+propWt="848." delays="6" auto-calc-mass="1" auto-calc-cg="1" avgThrust="157.444"\r
+peakThrust="272.248" throatDia="0." exitDia="0." Itot="1523.9" burn-time="9.68"\r
+massFrac="57.61" Isp="183.25" tDiv="10" tStep="-1." tFix="1" FDiv="10"\r
+FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."\r
+cgFix="1">\r
+ <comments>Pro54 4G 1526 K160-CL 6</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="848." cg="202."/>\r
+ <eng-data t="0.027" f="160.187" m="846.797" cg="202."/>\r
+ <eng-data t="0.08" f="242.037" m="840.865" cg="202."/>\r
+ <eng-data t="0.321" f="260.656" m="807.157" cg="202."/>\r
+ <eng-data t="0.455" f="259.602" m="787.76" cg="202."/>\r
+ <eng-data t="0.957" f="270.492" m="713.72" cg="202."/>\r
+ <eng-data t="1.593" f="272.248" m="617.679" cg="202."/>\r
+ <eng-data t="2.102" f="265.222" m="541.562" cg="202."/>\r
+ <eng-data t="2.564" f="254.333" m="474.776" cg="202."/>\r
+ <eng-data t="2.925" f="239.578" m="425.166" cg="202."/>\r
+ <eng-data t="3.956" f="190.047" m="301.924" cg="202."/>\r
+ <eng-data t="5.301" f="138.759" m="178.877" cg="202."/>\r
+ <eng-data t="7.617" f="67.799" m="45.7728" cg="202."/>\r
+ <eng-data t="9.19" f="25.644" m="4.87637" cg="202."/>\r
+ <eng-data t="9.572" f="15.808" m="0.470621" cg="202."/>\r
+ <eng-data t="9.679" f="0." m="0." cg="202."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="K1620-Vmax" Type="unspecified" dia="98." len="240."\r
+initWt="3077." propWt="1212." delays="0" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="1589.1" peakThrust="1844.79" throatDia="0." exitDia="0."\r
+Itot="2432.91" burn-time="1.531" massFrac="39.389" Isp="204.693" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="1212." cg="120."/>\r
+ <eng-data t="0.01" f="29.61" m="1211.93" cg="120."/>\r
+ <eng-data t="0.02" f="199.21" m="1211.36" cg="120."/>\r
+ <eng-data t="0.03" f="1107.95" m="1208.1" cg="120."/>\r
+ <eng-data t="0.04" f="1271.78" m="1202.17" cg="120."/>\r
+ <eng-data t="0.05" f="1403.3" m="1195.51" cg="120."/>\r
+ <eng-data t="0.06" f="1327.92" m="1188.71" cg="120."/>\r
+ <eng-data t="0.07" f="1440.22" m="1181.81" cg="120."/>\r
+ <eng-data t="0.08" f="1436.37" m="1174.65" cg="120."/>\r
+ <eng-data t="0.08" f="1827.48" m="1174.65" cg="120."/>\r
+ <eng-data t="0.09" f="1418.68" m="1166.56" cg="120."/>\r
+ <eng-data t="0.1" f="1474.45" m="1159.35" cg="120."/>\r
+ <eng-data t="0.2" f="1569.82" m="1083.53" cg="120."/>\r
+ <eng-data t="0.3" f="1660.96" m="1003.05" cg="120."/>\r
+ <eng-data t="0.4" f="1742.49" m="918.278" cg="120."/>\r
+ <eng-data t="0.5" f="1782.1" m="830.486" cg="120."/>\r
+ <eng-data t="0.6" f="1815.94" m="740.864" cg="120."/>\r
+ <eng-data t="0.7" f="1844.79" m="649.681" cg="120."/>\r
+ <eng-data t="0.9" f="1795.56" m="468.33" cg="120."/>\r
+ <eng-data t="1." f="1779.41" m="379.283" cg="120."/>\r
+ <eng-data t="1.1" f="1723.26" m="292.036" cg="120."/>\r
+ <eng-data t="1.2" f="1652.12" m="207.961" cg="120."/>\r
+ <eng-data t="1.3" f="1533.28" m="128.617" cg="120."/>\r
+ <eng-data t="1.35" f="1486.75" m="91.0052" cg="120."/>\r
+ <eng-data t="1.4" f="1451.37" m="54.4131" cg="120."/>\r
+ <eng-data t="1.45" f="1261.78" m="20.6229" cg="120."/>\r
+ <eng-data t="1.46" f="1111.03" m="14.7126" cg="120."/>\r
+ <eng-data t="1.47" f="929.51" m="9.62995" cg="120."/>\r
+ <eng-data t="1.48" f="628." m="5.75043" cg="120."/>\r
+ <eng-data t="1.49" f="382.26" m="3.23403" cg="120."/>\r
+ <eng-data t="1.5" f="223.44" m="1.72532" cg="120."/>\r
+ <eng-data t="1.531" f="0." m="0." cg="120."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="K1720ST" Type="reloadable" dia="54."\r
+len="403." initWt="1500." propWt="592." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="1730.35" peakThrust="1928.26" throatDia="0."\r
+exitDia="0." Itot="1183.56" burn-time="0.68" massFrac="39.47" Isp="203.87"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve from the AMW web site and CAR/NAR/TRA certified\r
+rocket motor list dated 9/28/08. The total weight was estimated based on\r
+similar motors such as the K455TT, K535RR and K665BB.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="592." cg="201.5"/>\r
+<eng-data t="0.007" f="1806.44" m="588.838" cg="201.5"/>\r
+<eng-data t="0.011" f="1608.04" m="585.422" cg="201.5"/>\r
+<eng-data t="0.016" f="1702.02" m="581.283" cg="201.5"/>\r
+<eng-data t="0.02" f="1514.07" m="578.065" cg="201.5"/>\r
+<eng-data t="0.024" f="1743.79" m="574.806" cg="201.5"/>\r
+<eng-data t="0.029" f="1541.91" m="570.698" cg="201.5"/>\r
+<eng-data t="0.032" f="1750.75" m="568.227" cg="201.5"/>\r
+<eng-data t="0.039" f="1597.6" m="562.365" cg="201.5"/>\r
+<eng-data t="0.042" f="1736.83" m="559.864" cg="201.5"/>\r
+<eng-data t="0.047" f="1691.58" m="555.577" cg="201.5"/>\r
+<eng-data t="0.05" f="1747.27" m="552.997" cg="201.5"/>\r
+<eng-data t="0.054" f="1715.94" m="549.532" cg="201.5"/>\r
+<eng-data t="0.058" f="1736.83" m="546.078" cg="201.5"/>\r
+<eng-data t="0.065" f="1771.63" m="539.936" cg="201.5"/>\r
+<eng-data t="0.072" f="1764.67" m="533.745" cg="201.5"/>\r
+<eng-data t="0.081" f="1823.84" m="525.668" cg="201.5"/>\r
+<eng-data t="0.09" f="1827.32" m="517.45" cg="201.5"/>\r
+<eng-data t="0.115" f="1858.65" m="494.404" cg="201.5"/>\r
+<eng-data t="0.137" f="1879.53" m="473.836" cg="201.5"/>\r
+<eng-data t="0.144" f="1869.09" m="467.274" cg="201.5"/>\r
+<eng-data t="0.148" f="1823.84" m="463.579" cg="201.5"/>\r
+<eng-data t="0.15" f="1844.72" m="461.744" cg="201.5"/>\r
+<eng-data t="0.17" f="1865.61" m="443.186" cg="201.5"/>\r
+<eng-data t="0.201" f="1886.49" m="414.096" cg="201.5"/>\r
+<eng-data t="0.234" f="1910.86" m="382.757" cg="201.5"/>\r
+<eng-data t="0.276" f="1917.82" m="342.54" cg="201.5"/>\r
+<eng-data t="0.312" f="1928.26" m="307.913" cg="201.5"/>\r
+<eng-data t="0.345" f="1921.3" m="276.142" cg="201.5"/>\r
+<eng-data t="0.384" f="1914.34" m="238.731" cg="201.5"/>\r
+<eng-data t="0.426" f="1886.49" m="198.807" cg="201.5"/>\r
+<eng-data t="0.487" f="1827.32" m="142.151" cg="201.5"/>\r
+<eng-data t="0.526" f="1792.51" m="106.844" cg="201.5"/>\r
+<eng-data t="0.555" f="1757.71" m="81.0954" cg="201.5"/>\r
+<eng-data t="0.575" f="1750.75" m="63.5466" cg="201.5"/>\r
+<eng-data t="0.593" f="1736.83" m="47.8466" cg="201.5"/>\r
+<eng-data t="0.604" f="1736.83" m="38.2905" cg="201.5"/>\r
+<eng-data t="0.615" f="1726.38" m="28.7632" cg="201.5"/>\r
+<eng-data t="0.621" f="1702.02" m="23.6187" cg="201.5"/>\r
+<eng-data t="0.624" f="1649.81" m="21.1038" cg="201.5"/>\r
+<eng-data t="0.628" f="1590.64" m="17.8622" cg="201.5"/>\r
+<eng-data t="0.631" f="1548.87" m="15.5067" cg="201.5"/>\r
+<eng-data t="0.643" f="964.129" m="7.96486" cg="201.5"/>\r
+<eng-data t="0.655" f="518.611" m="3.51499" cg="201.5"/>\r
+<eng-data t="0.666" f="268.007" m="1.35098" cg="201.5"/>\r
+<eng-data t="0.674" f="180.992" m="0.452649" cg="201.5"/>\r
+<eng-data t="0.684" f="0." m="0." cg="201.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+;Cesaroni Pro54 K2045 Vmax\r
+;By Karl Baumheckel\r
+;from rocksim file by Thomas Raithby 11/28/09\r
+K2045Vmax 54 404 7-10-13-15-17 0.716 1.290 CTI\r
+0.01 1165.25\r
+0.02 1854.79\r
+0.03 1907.47\r
+0.04 1947.47\r
+0.05 1944.77\r
+0.06 1970.16\r
+0.07 1994.77\r
+0.08 1998.62\r
+0.09 2018.23\r
+0.1 2034.77\r
+0.15 2042.46\r
+0.2 2138.98\r
+0.3 2183.98\r
+0.4 2164.75\r
+0.5 2148.98\r
+0.6 2154.75\r
+0.65 2091.91\r
+0.67 1507.52\r
+0.68 982.58\r
+0.69 481.87\r
+0.7 184.59\r
+0.72 36.15\r
+0.734 0\r
+;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="K2045-Vmax" Type="unspecified" dia="54." len="404."\r
+initWt="1290." propWt="725." delays="17,15,13,10,7" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="1931.18" peakThrust="2183.98" throatDia="0."\r
+exitDia="0." Itot="1417.49" burn-time="0.734" massFrac="56.2016" Isp="199.37"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="725." cg="202."/>\r
+ <eng-data t="0.01" f="1165.25" m="722.02" cg="202."/>\r
+ <eng-data t="0.02" f="1854.79" m="714.297" cg="202."/>\r
+ <eng-data t="0.03" f="1907.47" m="704.675" cg="202."/>\r
+ <eng-data t="0.04" f="1947.47" m="694.817" cg="202."/>\r
+ <eng-data t="0.05" f="1944.77" m="684.863" cg="202."/>\r
+ <eng-data t="0.06" f="1970.16" m="674.851" cg="202."/>\r
+ <eng-data t="0.07" f="1994.77" m="664.712" cg="202."/>\r
+ <eng-data t="0.08" f="1998.62" m="654.499" cg="202."/>\r
+ <eng-data t="0.09" f="2018.23" m="644.227" cg="202."/>\r
+ <eng-data t="0.1" f="2034.77" m="633.862" cg="202."/>\r
+ <eng-data t="0.15" f="2042.46" m="581.728" cg="202."/>\r
+ <eng-data t="0.2" f="2138.98" m="528.261" cg="202."/>\r
+ <eng-data t="0.3" f="2183.98" m="417.708" cg="202."/>\r
+ <eng-data t="0.4" f="2164.75" m="306.496" cg="202."/>\r
+ <eng-data t="0.5" f="2148.98" m="196.179" cg="202."/>\r
+ <eng-data t="0.6" f="2154.75" m="86.1179" cg="202."/>\r
+ <eng-data t="0.62" f="2121.29" m="64.2474" cg="202."/>\r
+ <eng-data t="0.63" f="2106.68" m="53.435" cg="202."/>\r
+ <eng-data t="0.65" f="2091.91" m="31.9605" cg="202."/>\r
+ <eng-data t="0.655" f="2038.61" m="26.6789" cg="202."/>\r
+ <eng-data t="0.67" f="1507.52" m="13.0759" cg="202."/>\r
+ <eng-data t="0.68" f="982.58" m="6.70791" cg="202."/>\r
+ <eng-data t="0.69" f="481.87" m="2.96281" cg="202."/>\r
+ <eng-data t="0.7" f="184.59" m="1.25844" cg="202."/>\r
+ <eng-data t="0.72" f="36.15" m="0.129427" cg="202."/>\r
+ <eng-data t="0.734" f="0." m="0." cg="202."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; Pro54 6G 2285 K260-CL P\r
+; Longburn\r
+K260-CL 54 572 P 1.2413 2.0475 CTI\r
+ 0.042 325.731\r
+ 0.101 430.409\r
+ 0.422 422.807\r
+ 0.773 426.901\r
+ 1.178 429.825\r
+ 1.517 425.731\r
+ 2.011 413.45\r
+ 3.195 356.725\r
+ 4.51 289.474\r
+ 6.015 174.269\r
+ 6.997 91.228\r
+ 7.366 66.667\r
+ 7.902 43.275\r
+ 8.479 25.731\r
+ 8.687 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="K300-CL" Type="unspecified" dia="54." len="649." initWt="2270."\r
+propWt="1377.6" delays="0" auto-calc-mass="1" auto-calc-cg="1" avgThrust="303.87"\r
+peakThrust="543.273" throatDia="0." exitDia="0." Itot="2543.39" burn-time="8.37"\r
+massFrac="60.69" Isp="188.26" tDiv="10" tStep="-1." tFix="1" FDiv="10"\r
+FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."\r
+cgFix="1">\r
+ <comments>Pro54 6GXL 2546 K300-CL P\r
+Longburn\r
+Uses a new threaded forward closure\r
+</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="1377.6" cg="324.5"/>\r
+ <eng-data t="0.036" f="495.273" m="1372.77" cg="324.5"/>\r
+ <eng-data t="0.132" f="543.273" m="1345.77" cg="324.5"/>\r
+ <eng-data t="0.265" f="506.909" m="1307.94" cg="324.5"/>\r
+ <eng-data t="0.734" f="493.091" m="1180.93" cg="324.5"/>\r
+ <eng-data t="1.258" f="489.455" m="1041.5" cg="324.5"/>\r
+ <eng-data t="1.811" f="482.909" m="895.873" cg="324.5"/>\r
+ <eng-data t="2.467" f="453.818" m="729.456" cg="324.5"/>\r
+ <eng-data t="3.737" f="375.273" m="444.298" cg="324.5"/>\r
+ <eng-data t="4.705" f="299.636" m="267.368" cg="324.5"/>\r
+ <eng-data t="6.047" f="165.091" m="98.4675" cg="324.5"/>\r
+ <eng-data t="6.474" f="120.727" m="65.4155" cg="324.5"/>\r
+ <eng-data t="6.829" f="90.182" m="45.1385" cg="324.5"/>\r
+ <eng-data t="7.323" f="63.273" m="24.6086" cg="324.5"/>\r
+ <eng-data t="7.72" f="46.545" m="12.8014" cg="324.5"/>\r
+ <eng-data t="8.309" f="30.545" m="0.504603" cg="324.5"/>\r
+ <eng-data t="8.37" f="0." m="0." cg="324.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="K400-GR" Type="unspecified" dia="54." len="404." initWt="1551.3"\r
+propWt="969." delays="14,13,12,11,10,9,8,7,6,5,4" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="397.016" peakThrust="475.4" throatDia="0."\r
+exitDia="0." Itot="1594.82" burn-time="4.02" massFrac="62.46" Isp="167.83"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Pro54 4G 1597 K400-GR 14A</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="969." cg="202."/>\r
+ <eng-data t="0.014" f="359.164" m="967.472" cg="202."/>\r
+ <eng-data t="0.102" f="475.4" m="945.161" cg="202."/>\r
+ <eng-data t="1.193" f="444.649" m="640.218" cg="202."/>\r
+ <eng-data t="2.807" f="384.994" m="233.42" cg="202."/>\r
+ <eng-data t="3.364" f="370.234" m="105.624" cg="202."/>\r
+ <eng-data t="3.599" f="363.469" m="53.2434" cg="202."/>\r
+ <eng-data t="3.693" f="329.028" m="33.4678" cg="202."/>\r
+ <eng-data t="3.859" f="169.742" m="8.31465" cg="202."/>\r
+ <eng-data t="3.967" f="57.196" m="0.868799" cg="202."/>\r
+ <eng-data t="4.017" f="0." m="0." cg="202."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-K445 54.0 404.00 7-17 0.79200 1.39800 CTI\r
- 0.05 664.83 \r
- 0.19 640.68 \r
- 0.48 622.98 \r
- 1.00 576.29 \r
- 1.51 515.12 \r
- 2.00 442.68 \r
- 2.50 392.26 \r
- 3.02 350.93 \r
- 3.13 339.66 \r
- 3.31 210.88 \r
- 3.47 78.88 \r
- 3.67 0.00 \r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="K445" Type="reloadable" dia="54."\r
+len="404." initWt="1398." propWt="826." delays="7,17" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="403.868" peakThrust="665.009" throatDia="0."\r
+exitDia="0." Itot="1635.67" burn-time="4.05" massFrac="59.08" Isp="201.93"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="826." cg="202."/>\r
+<eng-data t="0.05" f="665.009" m="817.604" cg="202."/>\r
+<eng-data t="0.1" f="599.62" m="801.639" cg="202."/>\r
+<eng-data t="0.2" f="624.975" m="770.718" cg="202."/>\r
+<eng-data t="0.4" f="620.527" m="707.821" cg="202."/>\r
+<eng-data t="0.5" f="616.078" m="676.597" cg="202."/>\r
+<eng-data t="1." f="576.044" m="526.094" cg="202."/>\r
+<eng-data t="1.5" f="515.994" m="388.226" cg="202."/>\r
+<eng-data t="2." f="449.27" m="266.363" cg="202."/>\r
+<eng-data t="2.5" f="395.892" m="159.663" cg="202."/>\r
+<eng-data t="3." f="353.633" m="65.0365" cg="202."/>\r
+<eng-data t="3.1" f="340.289" m="47.5152" cg="202."/>\r
+<eng-data t="3.15" f="342.513" m="38.895" cg="202."/>\r
+<eng-data t="3.2" f="293.583" m="30.8644" cg="202."/>\r
+<eng-data t="3.3" f="191.273" m="18.6219" cg="202."/>\r
+<eng-data t="3.45" f="77.843" m="8.42931" cg="202."/>\r
+<eng-data t="3.6" f="51.155" m="3.54357" cg="202."/>\r
+<eng-data t="3.7" f="26.689" m="1.57804" cg="202."/>\r
+<eng-data t="3.8" f="10.231" m="0.645823" cg="202."/>\r
+<eng-data t="4.05" f="0." m="0." cg="202."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+K454-SK 54 404 10-11-12-13-14-15-16-17-18-19 0.821 1.391 CTI \r
+0.021 10\r
+0.028 421\r
+0.032 586\r
+0.069 405\r
+0.2 475\r
+0.4 510\r
+0.6 530\r
+0.9 532\r
+1.2 525\r
+1.6 505\r
+2 470\r
+2.4 415\r
+2.55 410\r
+2.69 430\r
+2.93 70\r
+3 27\r
+3.15 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="K455TT" Type="reloadable" dia="54."\r
+len="403." initWt="1504." propWt="716." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="457.266" peakThrust="789.038" throatDia="0."\r
+exitDia="0." Itot="1481.54" burn-time="3.24" massFrac="47.61" Isp="211."\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John\r
+Coker. Data from CAR web site, thrust curve from AMW web site.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="716." cg="201.5"/>\r
+<eng-data t="0.021" f="715.739" m="712.368" cg="201.5"/>\r
+<eng-data t="0.035" f="789.038" m="707.277" cg="201.5"/>\r
+<eng-data t="0.052" f="735.861" m="701.013" cg="201.5"/>\r
+<eng-data t="0.069" f="689.869" m="695.157" cg="201.5"/>\r
+<eng-data t="0.09" f="684.12" m="688.184" cg="201.5"/>\r
+<eng-data t="0.114" f="681.246" m="680.266" cg="201.5"/>\r
+<eng-data t="0.138" f="691.307" m="672.306" cg="201.5"/>\r
+<eng-data t="0.19" f="682.683" m="655.042" cg="201.5"/>\r
+<eng-data t="0.345" f="663.999" m="604.603" cg="201.5"/>\r
+<eng-data t="0.528" f="645.315" m="546.705" cg="201.5"/>\r
+<eng-data t="0.583" f="641.004" m="529.609" cg="201.5"/>\r
+<eng-data t="0.735" f="625.194" m="483.103" cg="201.5"/>\r
+<eng-data t="0.835" f="616.571" m="453.097" cg="201.5"/>\r
+<eng-data t="0.983" f="589.263" m="409.973" cg="201.5"/>\r
+<eng-data t="1.163" f="567.705" m="359.65" cg="201.5"/>\r
+<eng-data t="1.304" f="544.709" m="321.749" cg="201.5"/>\r
+<eng-data t="1.598" f="492.969" m="248.03" cg="201.5"/>\r
+<eng-data t="1.663" f="480.034" m="232.747" cg="201.5"/>\r
+<eng-data t="1.932" f="434.043" m="173.331" cg="201.5"/>\r
+<eng-data t="1.984" f="426.857" m="162.514" cg="201.5"/>\r
+<eng-data t="2.019" f="426.857" m="155.293" cg="201.5"/>\r
+<eng-data t="2.077" f="408.173" m="143.59" cg="201.5"/>\r
+<eng-data t="2.119" f="405.298" m="135.334" cg="201.5"/>\r
+<eng-data t="2.157" f="399.549" m="127.944" cg="201.5"/>\r
+<eng-data t="2.205" f="388.052" m="118.809" cg="201.5"/>\r
+<eng-data t="2.232" f="386.614" m="113.755" cg="201.5"/>\r
+<eng-data t="2.315" f="369.368" m="98.5927" cg="201.5"/>\r
+<eng-data t="2.364" f="363.619" m="89.9139" cg="201.5"/>\r
+<eng-data t="2.398" f="360.744" m="83.9627" cg="201.5"/>\r
+<eng-data t="2.433" f="346.372" m="77.9823" cg="201.5"/>\r
+<eng-data t="2.481" f="340.623" m="70.0141" cg="201.5"/>\r
+<eng-data t="2.522" f="333.437" m="63.336" cg="201.5"/>\r
+<eng-data t="2.636" f="306.13" m="45.7179" cg="201.5"/>\r
+<eng-data t="2.705" f="286.008" m="35.845" cg="201.5"/>\r
+<eng-data t="2.753" f="267.324" m="29.4271" cg="201.5"/>\r
+<eng-data t="2.802" f="240.017" m="23.42" cg="201.5"/>\r
+<eng-data t="2.85" f="206.961" m="18.2356" cg="201.5"/>\r
+<eng-data t="2.916" f="159.532" m="12.3907" cg="201.5"/>\r
+<eng-data t="3.012" f="106.355" m="6.22278" cg="201.5"/>\r
+<eng-data t="3.081" f="79.048" m="3.13153" cg="201.5"/>\r
+<eng-data t="3.164" f="40.242" m="0.73903" cg="201.5"/>\r
+<eng-data t="3.24" f="0." m="0." cg="201.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="K490-GR" Type="unspecified" dia="54." len="488." initWt="1854.1"\r
+propWt="1201.2" delays="16,15,14,13,12,11,10,9,8,7,6" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="488.864" peakThrust="593.796" throatDia="0."\r
+exitDia="0." Itot="1987.72" burn-time="4.07" massFrac="64.79" Isp="168.74"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Pro54-5G 1990K490-GR 16A</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="1201.2" cg="244."/>\r
+ <eng-data t="0.013" f="445.79" m="1199.45" cg="244."/>\r
+ <eng-data t="0.024" f="376.662" m="1196.72" cg="244."/>\r
+ <eng-data t="0.083" f="559.232" m="1180.03" cg="244."/>\r
+ <eng-data t="0.121" f="584.047" m="1166.9" cg="244."/>\r
+ <eng-data t="0.316" f="573.412" m="1098.71" cg="244."/>\r
+ <eng-data t="0.727" f="569.867" m="956.727" cg="244."/>\r
+ <eng-data t="1.116" f="553.914" m="824.64" cg="244."/>\r
+ <eng-data t="1.875" f="522.009" m="577.893" cg="244."/>\r
+ <eng-data t="1.893" f="593.796" m="571.824" cg="244."/>\r
+ <eng-data t="1.944" f="519.35" m="554.671" cg="244."/>\r
+ <eng-data t="2.658" f="479.468" m="339.187" cg="244."/>\r
+ <eng-data t="3.063" f="473.264" m="222.599" cg="244."/>\r
+ <eng-data t="3.358" f="444.018" m="140.836" cg="244."/>\r
+ <eng-data t="3.618" f="448.449" m="70.7237" cg="244."/>\r
+ <eng-data t="3.894" f="240.177" m="13.296" cg="244."/>\r
+ <eng-data t="4.055" f="31.019" m="0.103098" cg="244."/>\r
+ <eng-data t="4.066" f="0." m="0." cg="244."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="K500-RL" Type="unspecified" dia="54." len="404." initWt="1476."\r
+propWt="904." delays="8,11,13,15,18" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="495.479" peakThrust="595.261" throatDia="0." exitDia="0."\r
+Itot="1587.02" burn-time="3.203" massFrac="61.2466" Isp="179.017" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="904." cg="202."/>\r
+ <eng-data t="0.01" f="11.873" m="903.966" cg="202."/>\r
+ <eng-data t="0.02" f="0.001" m="903.932" cg="202."/>\r
+ <eng-data t="0.03" f="292.263" m="903.1" cg="202."/>\r
+ <eng-data t="0.04" f="374.727" m="901.2" cg="202."/>\r
+ <eng-data t="0.05" f="432.875" m="898.9" cg="202."/>\r
+ <eng-data t="0.06" f="479.835" m="896.301" cg="202."/>\r
+ <eng-data t="0.07" f="505.514" m="893.494" cg="202."/>\r
+ <eng-data t="0.08" f="509.535" m="890.603" cg="202."/>\r
+ <eng-data t="0.09" f="584.943" m="887.486" cg="202."/>\r
+ <eng-data t="0.1" f="499.028" m="884.399" cg="202."/>\r
+ <eng-data t="0.2" f="546.632" m="854.617" cg="202."/>\r
+ <eng-data t="0.3" f="579.861" m="822.534" cg="202."/>\r
+ <eng-data t="0.4" f="588.092" m="789.269" cg="202."/>\r
+ <eng-data t="0.5" f="595.261" m="755.566" cg="202."/>\r
+ <eng-data t="0.6" f="594.616" m="721.677" cg="202."/>\r
+ <eng-data t="0.7" f="594.464" m="687.811" cg="202."/>\r
+ <eng-data t="0.8" f="593.82" m="653.967" cg="202."/>\r
+ <eng-data t="0.9" f="584.943" m="620.395" cg="202."/>\r
+ <eng-data t="1." f="583.274" m="587.123" cg="202."/>\r
+ <eng-data t="1.1" f="575.309" m="554.125" cg="202."/>\r
+ <eng-data t="1.2" f="568.064" m="521.561" cg="202."/>\r
+ <eng-data t="1.3" f="564.347" m="489.308" cg="202."/>\r
+ <eng-data t="1.4" f="560.288" m="457.278" cg="202."/>\r
+ <eng-data t="1.5" f="540.336" m="425.931" cg="202."/>\r
+ <eng-data t="1.6" f="543.067" m="395.074" cg="202."/>\r
+ <eng-data t="1.7" f="532.56" m="364.439" cg="202."/>\r
+ <eng-data t="1.8" f="532.494" m="334.105" cg="202."/>\r
+ <eng-data t="1.9" f="508.625" m="304.453" cg="202."/>\r
+ <eng-data t="2." f="505.401" m="275.573" cg="202."/>\r
+ <eng-data t="2.1" f="496.335" m="247.042" cg="202."/>\r
+ <eng-data t="2.2" f="483.893" m="219.124" cg="202."/>\r
+ <eng-data t="2.3" f="476.307" m="191.777" cg="202."/>\r
+ <eng-data t="2.4" f="467.014" m="164.91" cg="202."/>\r
+ <eng-data t="2.5" f="454.762" m="138.657" cg="202."/>\r
+ <eng-data t="2.6" f="454.345" m="112.764" cg="202."/>\r
+ <eng-data t="2.7" f="437.882" m="87.3528" cg="202."/>\r
+ <eng-data t="2.8" f="436.062" m="62.4619" cg="202."/>\r
+ <eng-data t="2.9" f="415.692" m="38.203" cg="202."/>\r
+ <eng-data t="3." f="327.653" m="17.0318" cg="202."/>\r
+ <eng-data t="3.1" f="133.178" m="3.90684" cg="202."/>\r
+ <eng-data t="3.203" f="0." m="0." cg="202."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; Cesaroni Pro75 2486K510 \r
-; 'Classic Propellant'\r
-;\r
-; RockSim file by Kathy Miller\r
-; wRasp Adaptation by Len Lekx\r
-;\r
-K510 75 350 0 1.19 2.59 CTI\r
-0.10 645.25 \r
-0.30 689.75 \r
-0.50 658.60 \r
-1.00 636.35 \r
-1.60 600.75 \r
-2.00 565.15 \r
-2.40 534.00 \r
-2.50 525.10 \r
-3.00 471.70 \r
-3.50 422.75 \r
-3.70 400.50 \r
-4.00 391.60 \r
-4.40 382.70 \r
-4.50 378.25 \r
-4.60 333.75 \r
-4.70 66.75 \r
-4.84 0.00 \r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="K510" Type="reloadable" dia="75."\r
+len="350." initWt="2590." propWt="1197." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="513.64" peakThrust="669.23" throatDia="0."\r
+exitDia="0." Itot="2486.02" burn-time="4.84" massFrac="46.22" Isp="211.78"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="1197." cg="175."/>\r
+<eng-data t="0.04" f="394.38" m="1193.2" cg="175."/>\r
+<eng-data t="0.07" f="617.68" m="1185.89" cg="175."/>\r
+<eng-data t="0.1" f="645.17" m="1176.77" cg="175."/>\r
+<eng-data t="0.21" f="658.16" m="1142.26" cg="175."/>\r
+<eng-data t="0.35" f="669.23" m="1097.52" cg="175."/>\r
+<eng-data t="0.53" f="667.72" m="1039.58" cg="175."/>\r
+<eng-data t="0.82" f="661.58" m="946.775" cg="175."/>\r
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+<eng-data t="1.72" f="588.46" m="677.099" cg="175."/>\r
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+<eng-data t="3.07" f="470.31" m="328.373" cg="175."/>\r
+<eng-data t="3.56" f="426.81" m="222.544" cg="175."/>\r
+<eng-data t="3.98" f="398.96" m="139.047" cg="175."/>\r
+<eng-data t="4.32" f="393.98" m="74.1419" cg="175."/>\r
+<eng-data t="4.48" f="380.63" m="44.3044" cg="175."/>\r
+<eng-data t="4.6" f="364.22" m="22.786" cg="175."/>\r
+<eng-data t="4.65" f="290.91" m="14.9" cg="175."/>\r
+<eng-data t="4.8" f="91.23" m="1.10014" cg="175."/>\r
+<eng-data t="4.83" f="45.82" m="0.11031" cg="175."/>\r
+<eng-data t="4.84" f="0." m="0." cg="175."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-K510 75.0 350.00 0 1.19700 2.59000 CTI\r
- 0.04 394.38 \r
- 0.07 617.68 \r
- 0.10 645.17 \r
- 0.21 658.16 \r
- 0.35 669.23 \r
- 0.53 667.72 \r
- 0.82 661.58 \r
- 1.18 626.92 \r
- 1.72 588.46 \r
- 2.15 557.69 \r
- 2.39 542.31 \r
- 2.90 492.86 \r
- 3.07 470.31 \r
- 3.56 426.81 \r
- 3.98 398.96 \r
- 4.32 393.98 \r
- 4.48 380.63 \r
- 4.60 364.22 \r
- 4.65 290.91 \r
- 4.80 91.23 \r
- 4.84 45.82 \r
- 4.84 0.00 \r
--- /dev/null
+K515-SK 54 488 6-7-8-9-10-11-12-13-14-15-16 1.013 1.654 CTI \r
+0.01 10\r
+0.02 250\r
+0.028 550\r
+0.035 710\r
+0.06 540\r
+0.065 530\r
+0.1 560\r
+0.25 600\r
+0.5 612\r
+0.75 612\r
+1.1 602\r
+1.5 578\r
+2 531\r
+2.6 460\r
+2.78 458\r
+2.85 450\r
+2.95 300\r
+3.03 200\r
+3.18 40\r
+3.35 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="K530-SS" Type="reloadable" dia="54."\r
+len="404." initWt="1639.8" propWt="1025." delays="6,16" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="529.642" peakThrust="596.4" throatDia="0."\r
+exitDia="0." Itot="1414.14" burn-time="2.67" massFrac="62.51" Isp="140.69"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="1025." cg="202."/>\r
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+<eng-data t="2.64" f="137.19" m="1.49157" cg="202."/>\r
+<eng-data t="2.67" f="0." m="0." cg="202."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="K535RR" Type="reloadable" dia="54."\r
+len="403." initWt="1559." propWt="764." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="529.945" peakThrust="629.683" throatDia="0."\r
+exitDia="0." Itot="1436.15" burn-time="2.71" massFrac="49.01" Isp="191.68"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John\r
+Coker. Data from CAR web site, thrust curve from AMW web site.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="764." cg="201.5"/>\r
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+<eng-data t="2.71" f="0." m="0." cg="201.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-K570 54.0 488.00 7-17 0.99000 1.68500 CTI\r
- 0.04 892.67 \r
- 0.50 797.99 \r
- 1.00 738.68 \r
- 1.50 659.37 \r
- 2.00 585.96 \r
- 2.50 512.88 \r
- 2.97 417.16 \r
- 3.20 224.79 \r
- 3.47 67.00 \r
- 3.59 0.00 \r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="K570" Type="reloadable" dia="54."\r
+len="488." initWt="1685." propWt="1033." delays="7,17" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="530.835" peakThrust="900.765" throatDia="0."\r
+exitDia="0." Itot="2070.26" burn-time="3.9" massFrac="61.31" Isp="204.36"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="1033." cg="244."/>\r
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+<eng-data t="0.075" f="818.472" m="1011.04" cg="244."/>\r
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+<eng-data t="3.5" f="68.947" m="5.27144" cg="244."/>\r
+<eng-data t="3.6" f="51.155" m="2.27506" cg="244."/>\r
+<eng-data t="3.7" f="13.345" m="0.665878" cg="244."/>\r
+<eng-data t="3.9" f="0." m="0." cg="244."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-K575SS 75 395 1000 1.803 3.143 Cesaroni\r
-0 16\r
-0.11 664.5\r
-0.43 620.2\r
-0.87 629\r
-1.3 637.92\r
-1.73 637.92\r
-2.17 629\r
-2.6 615.77\r
-3.03 553.75\r
-3.47 518.31\r
-3.9 438.57\r
-4.18 79.74\r
-4.33 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="K575SS" Type="reloadable" dia="75."\r
+len="395." initWt="3143." propWt="1803." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="550.212" peakThrust="664.5" throatDia="0."\r
+exitDia="0." Itot="2382.42" burn-time="4.33" massFrac="57.37" Isp="134.74"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
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+<eng-data t="0.11" f="664.5" m="1774.68" cg="197.5"/>\r
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+<eng-data t="1.73" f="637.92" m="997.395" cg="197.5"/>\r
+<eng-data t="2.17" f="629." m="786.459" cg="197.5"/>\r
+<eng-data t="2.6" f="615.77" m="583.922" cg="197.5"/>\r
+<eng-data t="3.03" f="553.75" m="393.629" cg="197.5"/>\r
+<eng-data t="3.47" f="518.31" m="215.136" cg="197.5"/>\r
+<eng-data t="3.9" f="438.57" m="59.4416" cg="197.5"/>\r
+<eng-data t="4.18" f="79.74" m="4.52601" cg="197.5"/>\r
+<eng-data t="4.33" f="0." m="0." cg="197.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="K590-DT" Type="unspecified" dia="54." len="572." initWt="1994."\r
+propWt="1239." delays="15,13,11,9,7" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="561.562" peakThrust="1812.1" throatDia="0." exitDia="0."\r
+Itot="2415.28" burn-time="4.301" massFrac="62.1364" Isp="198.781" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Dual-Thrust</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="1239." cg="286."/>\r
+ <eng-data t="0.01" f="2.69" m="1238.99" cg="286."/>\r
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+ <eng-data t="0.4" f="1392.92" m="953.141" cg="286."/>\r
+ <eng-data t="0.5" f="1373.69" m="882.18" cg="286."/>\r
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+ <eng-data t="0.9" f="525.32" m="688.294" cg="286."/>\r
+ <eng-data t="1." f="526.09" m="661.326" cg="286."/>\r
+ <eng-data t="1.1" f="516.86" m="634.575" cg="286."/>\r
+ <eng-data t="1.2" f="520.32" m="607.973" cg="286."/>\r
+ <eng-data t="1.4" f="518.02" m="554.707" cg="286."/>\r
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+ <eng-data t="2.6" f="461.49" m="256.362" cg="286."/>\r
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+ <eng-data t="3.7" f="204.59" m="29.4919" cg="286."/>\r
+ <eng-data t="3.9" f="118.83" m="12.901" cg="286."/>\r
+ <eng-data t="4." f="89.22" m="7.56463" cg="286."/>\r
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+ <eng-data t="4.301" f="0." m="0." cg="286."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; Skidmark\r
+K610-SK 54 491 0 0.866 1.765 AMW/ProX \r
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--- /dev/null
+; CTI Pro54-4G 1679 K630BS 15A\r
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+ 0.025 676.277\r
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+ 2.816 0.0\r
--- /dev/null
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-K650SS 54.0 488.00 6-16 1.28100 1.98990 CTI\r
- 0.04 664.52 \r
- 0.12 645.90 \r
- 0.31 642.24 \r
- 0.60 664.78 \r
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- 2.66 0.00 \r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="K650SS" Type="reloadable" dia="54."\r
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+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-K660 54.0 572.00 7-17 1.17700 1.94900 CTI\r
- 0.07 1078.90 \r
- 0.23 1006.47 \r
- 0.40 966.76 \r
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- 3.01 386.90 \r
- 3.20 234.31 \r
- 3.45 106.65 \r
- 3.60 44.03 \r
- 3.69 0.00 \r
--- /dev/null
+<engine-database>\r
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+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="K665BB" Type="reloadable" dia="54."\r
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+<comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John\r
+Coker. Data from CAR web site, thrust curve from AMW web site.\r
+</comments>\r
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+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="K671RR" Type="reloadable" dia="54."\r
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+<comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John\r
+Coker. Data from CAR web site, thrust curve from AMW web site.\r
+</comments>\r
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+<eng-data t="2.474" f="259.596" m="11.2505" cg="245.5"/>\r
+<eng-data t="2.52" f="171.193" m="5.99967" cg="245.5"/>\r
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+<eng-data t="2.645" f="0." m="0." cg="245.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+K675-SK 54 572 8-9-10-11-12-13-14-15-16-17-18 1.2 1.94 CTI \r
+0.01 10\r
+0.02 154\r
+0.025 930\r
+0.04 850\r
+0.05 800\r
+0.07 680\r
+0.1 700\r
+0.2 750\r
+0.3 780\r
+0.5 795\r
+1 808\r
+1.5 795\r
+1.9 751\r
+2.26 700\r
+2.43 450\r
+2.6 440\r
+2.68 400\r
+2.96 40\r
+3.09 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="K701BB" Type="reloadable" dia="54."\r
+len="491." initWt="2088." propWt="1205." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="697.011" peakThrust="840.686" throatDia="0."\r
+exitDia="0." Itot="1658.19" burn-time="2.38" massFrac="57.71" Isp="140.32"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John\r
+Coker. Data from CAR web site, thrust curve from AMW web site.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="1205." cg="245.5"/>\r
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+<eng-data t="2.379" f="0." m="0." cg="245.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+K710-BB 54 491 0 0.902 1.812 AMW/ProX \r
+0.01 500\r
+0.02 850\r
+0.025 910\r
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+1.95 720\r
+2.2 295\r
+2.37 280\r
+2.5 90\r
+2.6 20\r
+2.8 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="K750" Type="reloadable" dia="54." len="573.3" initWt="2057."\r
+propWt="1321." delays="8,9,10,11,12,13,14,15,16,17,18" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="724.886" peakThrust="947.04" throatDia="0."\r
+exitDia="0." Itot="2311.66" burn-time="3.19" massFrac="64.22" Isp="178.44"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="1321." cg="286.65"/>\r
+ <eng-data t="0.019" f="796.375" m="1316.68" cg="286.65"/>\r
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+ <eng-data t="1.854" f="817.899" m="382.431" cg="286.65"/>\r
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+ <eng-data t="2.398" f="674.408" m="139.815" cg="286.65"/>\r
+ <eng-data t="2.521" f="516.567" m="97.9589" cg="286.65"/>\r
+ <eng-data t="2.599" f="509.393" m="75.0938" cg="286.65"/>\r
+ <eng-data t="2.878" f="243.935" m="15.0405" cg="286.65"/>\r
+ <eng-data t="2.962" f="121.967" m="6.25851" cg="286.65"/>\r
+ <eng-data t="3.059" f="50.222" m="1.48623" cg="286.65"/>\r
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+ <eng-data t="3.189" f="0." m="0." cg="286.65"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; CTI Pro54-5G 2108 J780BS 15A\r
+K780BS 54 489 15-14-13-12-11-10-9-8-7-6-5 1.1400000000000001 1.7 CTI\r
+ 0.0080 15.972\r
+ 0.016 511.106\r
+ 0.017 1014.226\r
+ 0.039 892.439\r
+ 0.065 936.362\r
+ 0.094 942.352\r
+ 0.153 916.397\r
+ 0.205 906.415\r
+ 0.294 914.401\r
+ 0.455 900.425\r
+ 0.718 896.432\r
+ 1.016 886.45\r
+ 1.38 858.498\r
+ 1.799 818.568\r
+ 1.913 804.593\r
+ 2.072 798.603\r
+ 2.225 788.621\r
+ 2.272 758.673\r
+ 2.34 606.938\r
+ 2.379 561.019\r
+ 2.412 495.134\r
+ 2.558 211.63\r
+ 2.628 141.752\r
+ 2.711 77.864\r
+ 2.756 0.0\r
--- /dev/null
+K815-SK 54 649 0 1.371 2.197 CTI \r
+0.01 400\r
+0.015 600\r
+0.02 1200\r
+0.05 620\r
+0.07 720\r
+0.1 825\r
+0.3 910\r
+1 945\r
+1.5 970\r
+1.8 970\r
+2.12 930\r
+2.3 650\r
+2.43 640\r
+2.58 300\r
+2.7 150\r
+2.85 0\r
--- /dev/null
+K820-BS 54 572 7-8-9-10-11-12-13-14-15-16-17 1.232 1.982 CTI \r
+0.01 800\r
+0.02 1400\r
+0.029 1720\r
+0.04 960\r
+0.1 1050\r
+0.2 1060\r
+0.4 1040\r
+0.6 1030\r
+1 1020\r
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+2 880\r
+2.1 800\r
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+2.3 520\r
+2.4 410\r
+2.5 390\r
+2.6 280\r
+2.7 180\r
+2.8 110\r
+2.9 50\r
+3 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="K855BB" Type="reloadable" dia="54."\r
+len="491." initWt="2121." propWt="1205." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="857.905" peakThrust="1021.66" throatDia="0."\r
+exitDia="0." Itot="1731.25" burn-time="2.02" massFrac="56.81" Isp="146.51"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John\r
+Coker. Data from CAR web site, thrust curve from AMW web site.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="1205." cg="245.5"/>\r
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+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="L1030-RL" Type="unspecified" dia="54." len="649." initWt="2338."\r
+propWt="1520." delays="0" auto-calc-mass="1" auto-calc-cg="1" avgThrust="1028.55"\r
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+cgFix="1">\r
+ <data>\r
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+ <eng-data t="2.6" f="258.432" m="9.32432" cg="324.5"/>\r
+ <eng-data t="2.7" f="79.606" m="0.0870133" cg="324.5"/>\r
+ <eng-data t="2.704" f="0." m="0." cg="324.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-L1090SS 75 665 1000 3.491 5.461 Cesaroni\r
-0 487.3\r
-0.11 1639.1\r
-0.22 1484.05\r
-0.44 1417.6\r
-0.87 1373.3\r
-1.31 1329\r
-1.74 1306.85\r
-2.18 1262.55\r
-2.61 1218.25\r
-3.05 1151.8\r
-3.21 775.25\r
-3.48 598.05\r
-3.92 553.75\r
-4.13 221.5\r
-4.35 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="L1090SS" Type="reloadable" dia="75."\r
+len="665." initWt="5461." propWt="3491." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="1077.69" peakThrust="1639.1" throatDia="0."\r
+exitDia="0." Itot="4687.94" burn-time="4.35" massFrac="63.93" Isp="136.93"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
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+<eng-data t="4.35" f="0." m="0." cg="332.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; Cesaroni Pro75 5015L1115\r
-; 'Classic Propellant'\r
-;\r
-; RockSim file by Kathy Miller\r
-; wRasp Adaptation by Len Lekx\r
-;\r
-L1115 75 621 0 2.39 4.40 CTI\r
-0.10 1468.85 \r
-0.30 1490.75 \r
-0.80 1401.75 \r
-1.00 1437.35 \r
-1.50 1335.00 \r
-2.00 1268.25 \r
-2.20 1246.00 \r
-2.50 1112.50 \r
-3.00 1090.25 \r
-3.30 979.00 \r
-3.80 979.00 \r
-4.00 623.00 \r
-4.20 311.50 \r
-4.40 35.00 \r
-4.48 0.00 \r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="L1115-Classic" Type="reloadable" dia="75."\r
+len="621." initWt="4404." propWt="2394." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="1093.26" peakThrust="1713.25" throatDia="0."\r
+exitDia="0." Itot="4908.73" burn-time="4.49" massFrac="54.36" Isp="209.09"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
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+<eng-data t="4.1" f="434.99" m="44.6817" cg="310.5"/>\r
+<eng-data t="4.22" f="288.73" m="23.5041" cg="310.5"/>\r
+<eng-data t="4.38" f="156.49" m="6.13332" cg="310.5"/>\r
+<eng-data t="4.48" f="86.39" m="0.210663" cg="310.5"/>\r
+<eng-data t="4.49" f="0." m="0." cg="310.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; AMX/ProX 2729L1276 RR\r
+L1276RR 54 728 P 1.475 2.96 AMW\r
+ 0.015 76.924\r
+ 0.017 692.317\r
+ 0.026 1495.003\r
+ 0.037 1244.164\r
+ 0.052 1401.357\r
+ 0.084 1307.71\r
+ 0.127 1307.71\r
+ 0.181 1367.911\r
+ 0.289 1401.357\r
+ 0.384 1408.046\r
+ 0.807 1421.424\r
+ 0.993 1461.558\r
+ 1.215 1491.659\r
+ 1.673 1474.936\r
+ 1.727 1384.634\r
+ 1.798 1083.627\r
+ 1.947 531.78\r
+ 1.986 351.175\r
+ 2.047 177.26\r
+ 2.092 93.647\r
+ 2.144 33.445\r
+ 2.185 0.0\r
--- /dev/null
+; ABC-76-6000 4701L1290-SK P\r
+L1290-SK 76 785 P 3.047 5.399 CTI\r
+ 0.022 117.623\r
+ 0.081 786.023\r
+ 0.11 797.226\r
+ 0.176 1226.645\r
+ 0.691 1357.337\r
+ 1.231 1461.891\r
+ 1.761 1476.828\r
+ 2.008 1467.493\r
+ 2.311 1417.082\r
+ 2.835 1299.459\r
+ 3.101 1235.98\r
+ 3.167 1230.379\r
+ 3.34 1321.863\r
+ 3.373 1286.39\r
+ 3.532 365.94\r
+ 3.602 201.64\r
+ 3.734 91.485\r
+ 3.782 69.08\r
+ 3.8 0.0\r
--- /dev/null
+L1355-SS 75 621 0 3.076 4.962 CTI \r
+0.1 80\r
+0.12 1300\r
+0.15 1600\r
+0.2 1500\r
+0.3 1540\r
+0.4 1560\r
+1.05 1660\r
+1.3 1750\r
+1.4 1750\r
+1.8 1590\r
+2.2 1270\r
+2.6 860\r
+2.82 680\r
+3.05 83\r
+3.25 0\r
--- /dev/null
+L1395-BS 75 621 0 2.475 4.323 CTI \r
+0.02 100\r
+0.04 1400\r
+0.1 1800\r
+0.2 1500\r
+0.4 1540\r
+0.8 1591\r
+1.1 1641\r
+2.4 1481\r
+2.8 1446\r
+3 1500\r
+3.18 830\r
+3.35 100\r
+3.45 0\r
--- /dev/null
+L1410-SK 75 757 P 2.875 5.115 CTI\r
+0.04 133\r
+0.065 1200\r
+0.077 1510\r
+0.13 1250\r
+0.35 1400\r
+1 1530\r
+1.5 1595\r
+2 1630\r
+2.3 1600\r
+2.6 1510\r
+2.9 1350\r
+3.25 1032\r
+3.4 120\r
+3.48 0\r
--- /dev/null
+L1685-SS 75 757 0 3.83 6.051 CTI \r
+0.055 100\r
+0.07 1000\r
+0.092 2300\r
+0.12 2150\r
+0.4 2150\r
+0.9 2050\r
+1.1 2060\r
+1.3 2150\r
+1.6 1900\r
+2.1 1600\r
+2.5 1150\r
+2.7 1000\r
+2.85 750\r
+3.02 200\r
+3.18 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="L1720-WT" Type="reloadable" dia="75."\r
+len="486." initWt="3341." propWt="1755." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="1735.86" peakThrust="1946.7" throatDia="0."\r
+exitDia="0." Itot="3695.65" burn-time="2.13" massFrac="52.53" Isp="214.73"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="1755." cg="243."/>\r
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+<eng-data t="2.08" f="557.24" m="4.93302" cg="243."/>\r
+<eng-data t="2.1" f="179.2" m="1.4358" cg="243."/>\r
+<eng-data t="2.12" f="84.93" m="0.181493" cg="243."/>\r
+<eng-data t="2.129" f="0." m="0." cg="243."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="L2375-WT" Type="reloadable" dia="75."\r
+len="621." initWt="4161." propWt="2321." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="2326.93" peakThrust="2608.28" throatDia="0."\r
+exitDia="0." Itot="4905.17" burn-time="2.11" massFrac="55.78" Isp="215.51"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>White Thunder</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="2321." cg="310.5"/>\r
+<eng-data t="0.01" f="18.15" m="2320.96" cg="310.5"/>\r
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+<eng-data t="2.108" f="0." m="0." cg="310.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="CTI" code="L3150-Vmax" Type="unspecified" dia="98." len="394."\r
+initWt="4807.8" propWt="2376." delays="0" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="3063.28" peakThrust="3656.89" throatDia="0." exitDia="0."\r
+Itot="4806.28" burn-time="1.569" massFrac="49.4197" Isp="206.273" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
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+ <eng-data t="1.1" f="3296.93" m="562.144" cg="197."/>\r
+ <eng-data t="1.2" f="3155.41" m="402.657" cg="197."/>\r
+ <eng-data t="1.3" f="2924.66" m="252.372" cg="197."/>\r
+ <eng-data t="1.4" f="2765.84" m="111.716" cg="197."/>\r
+ <eng-data t="1.45" f="2346.27" m="48.5362" cg="197."/>\r
+ <eng-data t="1.47" f="1629.43" m="28.8822" cg="197."/>\r
+ <eng-data t="1.5" f="883.36" m="10.2491" cg="197."/>\r
+ <eng-data t="1.52" f="411.88" m="3.84607" cg="197."/>\r
+ <eng-data t="1.55" f="65.38" m="0.307048" cg="197."/>\r
+ <eng-data t="1.569" f="0." m="0." cg="197."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+L585-IM 75 350 0 1.524 2.784 CTI \r
+0.01 200\r
+0.02 300\r
+0.04 500\r
+0.08 630\r
+0.1 650\r
+0.25 629\r
+0.4 639\r
+0.8 648\r
+1.2 654\r
+1.6 659\r
+2 653\r
+2.4 640\r
+2.8 610\r
+3.2 580\r
+3.6 550\r
+4 515\r
+4.2 510\r
+4.45 110\r
+4.57 0\r
+++ /dev/null
-;\r
-;\r
-L610 98 394 0 2.415 4.975 CTI \r
-0.06 262.5\r
-0.12 667.2\r
-0.25 929.7\r
-0.39 871.21\r
-0.65 849.83\r
-1.05 823.1\r
-1.5 785.69\r
-2 747.3\r
-2.5 707.3\r
-3 667.2\r
-3.48 641.38\r
-4 593.28\r
-4.47 561.21\r
-5 523.79\r
-5.44 502.41\r
-5.68 491.72\r
-6 475.69\r
-6.5 459.66\r
-7.01 443.62\r
-7.5 413.7\r
-8 284.7\r
-8.12 53.3\r
-8.13 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="L610" Type="reloadable" dia="98."\r
+len="427." initWt="4840." propWt="2415." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="595.595" peakThrust="929.678" throatDia="0."\r
+exitDia="0." Itot="4842.19" burn-time="8.13" massFrac="49.9" Isp="204.46"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Data Entered by Tim Van Milligan based on RMS case weight.\r
+Based on CAR certification data\r
+This data has not been approved by Cesaroni or Canadian Association of Rocketry.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="2415." cg="213.5"/>\r
+<eng-data t="0.155" f="929.678" m="2379.07" cg="213.5"/>\r
+<eng-data t="0.247" f="913.867" m="2336.77" cg="213.5"/>\r
+<eng-data t="0.355" f="891.846" m="2288.14" cg="213.5"/>\r
+<eng-data t="0.433" f="880.836" m="2253.66" cg="213.5"/>\r
+<eng-data t="0.618" f="897.352" m="2171.62" cg="213.5"/>\r
+<eng-data t="1.005" f="913.867" m="1996.83" cg="213.5"/>\r
+<eng-data t="1.87" f="902.857" m="1604.95" cg="213.5"/>\r
+<eng-data t="2.179" f="880.836" m="1467.51" cg="213.5"/>\r
+<eng-data t="2.411" f="875.331" m="1365.91" cg="213.5"/>\r
+<eng-data t="3.044" f="809.268" m="1099.99" cg="213.5"/>\r
+<eng-data t="3.988" f="677.143" m="750.081" cg="213.5"/>\r
+<eng-data t="4.853" f="550.523" m="485.267" cg="213.5"/>\r
+<eng-data t="5.502" f="500.975" m="315.091" cg="213.5"/>\r
+<eng-data t="5.889" f="473.449" m="221.052" cg="213.5"/>\r
+<eng-data t="6.306" f="456.934" m="124.304" cg="213.5"/>\r
+<eng-data t="6.507" f="401.881" m="81.2573" cg="213.5"/>\r
+<eng-data t="6.94" f="110.105" m="25.9743" cg="213.5"/>\r
+<eng-data t="7.172" f="66.063" m="15.7823" cg="213.5"/>\r
+<eng-data t="8.13" f="0." m="0." cg="213.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+L640-DT 54 649 P 1.293 2.244 CTI\r
+0.02 1200\r
+0.034 1540\r
+0.07 1300\r
+0.15 1460\r
+0.35 1510\r
+0.65 1540\r
+0.7 1510\r
+0.79 800\r
+0.86 570.25\r
+3.26 518\r
+3.55 330\r
+3.65 318\r
+4.15 102\r
+4.5 30\r
+5 0\r
+++ /dev/null
-;\r
-;\r
-L730 54.0 649.00 0 1.35100 2.24700 CTI\r
- 0.00 81.36 \r
- 0.01 1079.71 \r
- 0.02 1216.59 \r
- 0.04 1154.68 \r
- 0.20 1127.51 \r
- 0.45 1055.11 \r
- 0.60 1028.17 \r
- 0.75 995.24 \r
- 1.00 959.33 \r
- 1.50 898.71 \r
- 2.00 830.70 \r
- 2.50 730.76 \r
- 2.60 592.55 \r
- 2.70 510.96 \r
- 2.90 487.88 \r
- 3.00 405.72 \r
- 3.10 299.80 \r
- 3.20 296.09 \r
- 3.30 251.85 \r
- 3.40 171.70 \r
- 3.50 165.26 \r
- 3.60 139.38 \r
- 3.65 117.77 \r
- 3.77 45.38 \r
- 3.77 0.00 \r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="L730" Type="reloadable" dia="54."\r
+len="6490." initWt="2247." propWt="1351." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="732.947" peakThrust="1216.59" throatDia="0."\r
+exitDia="0." Itot="2763.21" burn-time="3.77" massFrac="60.12" Isp="208.56"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="1351." cg="3245."/>\r
+<eng-data t="0." f="81.36" m="1351." cg="3245."/>\r
+<eng-data t="0.01" f="1079.71" m="1348.16" cg="3245."/>\r
+<eng-data t="0.02" f="1216.59" m="1342.55" cg="3245."/>\r
+<eng-data t="0.04" f="1154.68" m="1330.95" cg="3245."/>\r
+<eng-data t="0.2" f="1127.51" m="1241.69" cg="3245."/>\r
+<eng-data t="0.45" f="1055.11" m="1108.3" cg="3245."/>\r
+<eng-data t="0.6" f="1028.17" m="1031.9" cg="3245."/>\r
+<eng-data t="0.75" f="995.24" m="957.708" cg="3245."/>\r
+<eng-data t="1." f="959.33" m="838.253" cg="3245."/>\r
+<eng-data t="1.5" f="898.71" m="611.143" cg="3245."/>\r
+<eng-data t="2." f="830.7" m="399.756" cg="3245."/>\r
+<eng-data t="2.5" f="730.76" m="208.897" cg="3245."/>\r
+<eng-data t="2.6" f="592.55" m="176.547" cg="3245."/>\r
+<eng-data t="2.7" f="510.96" m="149.571" cg="3245."/>\r
+<eng-data t="2.9" f="487.88" m="100.735" cg="3245."/>\r
+<eng-data t="3." f="405.72" m="78.8898" cg="3245."/>\r
+<eng-data t="3.1" f="299.8" m="61.6425" cg="3245."/>\r
+<eng-data t="3.2" f="296.09" m="47.0752" cg="3245."/>\r
+<eng-data t="3.3" f="251.85" m="33.6802" cg="3245."/>\r
+<eng-data t="3.4" f="171.7" m="23.326" cg="3245."/>\r
+<eng-data t="3.5" f="165.26" m="15.0886" cg="3245."/>\r
+<eng-data t="3.6" f="139.38" m="7.64134" cg="3245."/>\r
+<eng-data t="3.65" f="117.77" m="4.49817" cg="3245."/>\r
+<eng-data t="3.76" f="45.38" m="0.110937" cg="3245."/>\r
+<eng-data t="3.77" f="0." m="0." cg="3245."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; Cesaroni Pro75 3757L800\r
-; 'Classic Propellant'\r
-;\r
-; RockSim file by Kathy Miller\r
-; wRasp Adaptation by Len Lekx\r
-;\r
-L800 75 486 0 1.79 3.51 CTI\r
-0.10 1023.50 \r
-0.20 1005.70 \r
-0.30 1023.50 \r
-0.50 1014.60 \r
-1.00 1010.15 \r
-1.50 1001.25 \r
-2.00 956.75 \r
-2.40 890.00 \r
-2.50 845.50 \r
-3.00 756.50 \r
-3.50 689.75 \r
-3.70 667.50 \r
-3.90 654.15 \r
-4.00 623.00 \r
-4.60 111.25 \r
-4.67 0.00 \r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="L800" Type="reloadable" dia="75."\r
+len="486." initWt="3511." propWt="1795." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="795.478" peakThrust="1285.54" throatDia="0."\r
+exitDia="0." Itot="3722.84" burn-time="4.68" massFrac="51.13" Isp="211.49"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="1795." cg="243."/>\r
+<eng-data t="0." f="27.28" m="1795." cg="243."/>\r
+<eng-data t="0.01" f="402.41" m="1793.96" cg="243."/>\r
+<eng-data t="0.1" f="1285.54" m="1757.34" cg="243."/>\r
+<eng-data t="0.12" f="1056.51" m="1746.05" cg="243."/>\r
+<eng-data t="0.26" f="1041.73" m="1675.23" cg="243."/>\r
+<eng-data t="0.71" f="1026.95" m="1450.81" cg="243."/>\r
+<eng-data t="1.28" f="998.38" m="1172.5" cg="243."/>\r
+<eng-data t="2.05" f="901.36" m="819.845" cg="243."/>\r
+<eng-data t="2.41" f="849.64" m="667.878" cg="243."/>\r
+<eng-data t="2.83" f="763.51" m="504.541" cg="243."/>\r
+<eng-data t="3.25" f="707.06" m="355.641" cg="243."/>\r
+<eng-data t="3.65" f="655.14" m="224.282" cg="243."/>\r
+<eng-data t="3.8" f="651.74" m="177.022" cg="243."/>\r
+<eng-data t="4." f="624.07" m="115.508" cg="243."/>\r
+<eng-data t="4.1" f="601.34" m="85.966" cg="243."/>\r
+<eng-data t="4.19" f="536.17" m="61.2852" cg="243."/>\r
+<eng-data t="4.31" f="415.67" m="33.7489" cg="243."/>\r
+<eng-data t="4.41" f="270.17" m="17.2147" cg="243."/>\r
+<eng-data t="4.52" f="140.2" m="6.33224" cg="243."/>\r
+<eng-data t="4.6" f="76.92" m="2.14479" cg="243."/>\r
+<eng-data t="4.65" f="54.94" m="0.555351" cg="243."/>\r
+<eng-data t="4.67" f="40.16" m="0.0968175" cg="243."/>\r
+<eng-data t="4.68" f="0." m="0." cg="243."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-L800 75.0 486.00 0 1.79500 3.51100 CTI\r
- 0.00 27.28 \r
- 0.01 402.41 \r
- 0.01 1285.54 \r
- 0.12 1056.51 \r
- 0.26 1041.73 \r
- 0.71 1026.95 \r
- 1.28 998.38 \r
- 2.05 901.36 \r
- 2.41 849.64 \r
- 2.83 763.51 \r
- 3.25 707.06 \r
- 3.65 655.14 \r
- 3.80 651.74 \r
- 4.00 624.07 \r
- 4.10 601.34 \r
- 4.19 536.17 \r
- 4.31 415.67 \r
- 4.41 270.17 \r
- 4.52 140.20 \r
- 4.60 76.92 \r
- 4.65 54.94 \r
- 4.67 40.16 \r
- 5.00 0.00 \r
+++ /dev/null
-;\r
-;\r
-L890SS 75 530 1000 2.671 4.346 Cesaroni\r
-0 20\r
-0.05 1151.8\r
-0.41 1054.34\r
-0.83 1045.48\r
-1.24 1036.62\r
-1.65 1027.76\r
-2.07 1018.9\r
-2.89 886\r
-3.31 775.25\r
-3.72 664.5\r
-3.98 177.2\r
-4.13 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="L890SS" Type="reloadable" dia="75."\r
+len="530." initWt="4346." propWt="2671." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="894.654" peakThrust="1151.8" throatDia="0."\r
+exitDia="0." Itot="3694.92" burn-time="4.13" massFrac="61.46" Isp="141.06"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="2671." cg="265."/>\r
+<eng-data t="0." f="20." m="2671." cg="265."/>\r
+<eng-data t="0.05" f="1151.8" m="2649.82" cg="265."/>\r
+<eng-data t="0.41" f="1054.34" m="2362.76" cg="265."/>\r
+<eng-data t="0.83" f="1045.48" m="2044." cg="265."/>\r
+<eng-data t="1.24" f="1036.62" m="1735.45" cg="265."/>\r
+<eng-data t="1.65" f="1027.76" m="1429.53" cg="265."/>\r
+<eng-data t="2.07" f="1018.9" m="1118.83" cg="265."/>\r
+<eng-data t="2.89" f="886." m="554.251" cg="265."/>\r
+<eng-data t="3.31" f="775.25" m="302.064" cg="265."/>\r
+<eng-data t="3.72" f="664.5" m="88.7059" cg="265."/>\r
+<eng-data t="3.98" f="177.2" m="9.60713" cg="265."/>\r
+<eng-data t="4.13" f="0." m="0." cg="265."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; Pro54-6GXL 3147L935-IM P\r
+L935-IM 54 649 P 1.7347000000000001 2.5420000000000003 CTI\r
+ 0.012 1582.739\r
+ 0.052 1365.5\r
+ 0.159 1278.04\r
+ 2.198 990.27\r
+ 2.514 719.427\r
+ 3.021 239.809\r
+ 3.104 160.813\r
+ 3.273 107.209\r
+ 3.3 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="L985TT" Type="reloadable" dia="54."\r
+len="491." initWt="2572." propWt="1295." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="996.381" peakThrust="1483.94" throatDia="0."\r
+exitDia="0." Itot="2678.27" burn-time="2.69" massFrac="50.35" Isp="210.89"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John\r
+Coker. Data from CAR web site, thrust curve from AMW web site.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="1295." cg="245.5"/>\r
+<eng-data t="0.017" f="1483.94" m="1288.9" cg="245.5"/>\r
+<eng-data t="0.033" f="1394.18" m="1277.77" cg="245.5"/>\r
+<eng-data t="0.061" f="1315.63" m="1259.42" cg="245.5"/>\r
+<eng-data t="0.081" f="1251.11" m="1247.01" cg="245.5"/>\r
+<eng-data t="0.103" f="1290.38" m="1233.5" cg="245.5"/>\r
+<eng-data t="0.134" f="1307.22" m="1214.03" cg="245.5"/>\r
+<eng-data t="0.17" f="1310.02" m="1191.25" cg="245.5"/>\r
+<eng-data t="0.27" f="1287.58" m="1128.45" cg="245.5"/>\r
+<eng-data t="0.396" f="1270.75" m="1050.52" cg="245.5"/>\r
+<eng-data t="0.485" f="1262.33" m="996.015" cg="245.5"/>\r
+<eng-data t="0.56" f="1231.48" m="950.798" cg="245.5"/>\r
+<eng-data t="0.618" f="1253.92" m="915.947" cg="245.5"/>\r
+<eng-data t="0.699" f="1242.7" m="867.057" cg="245.5"/>\r
+<eng-data t="0.827" f="1220.26" m="790.84" cg="245.5"/>\r
+<eng-data t="1.087" f="1178.18" m="640.08" cg="245.5"/>\r
+<eng-data t="1.273" f="1158.54" m="535.004" cg="245.5"/>\r
+<eng-data t="1.443" f="1136.1" m="440.696" cg="245.5"/>\r
+<eng-data t="1.619" f="1119.27" m="344.731" cg="245.5"/>\r
+<eng-data t="1.755" f="1096.83" m="271.867" cg="245.5"/>\r
+<eng-data t="1.83" f="1091.22" m="232.193" cg="245.5"/>\r
+<eng-data t="1.878" f="1085.61" m="206.932" cg="245.5"/>\r
+<eng-data t="1.917" f="1082.8" m="186.487" cg="245.5"/>\r
+<eng-data t="1.942" f="1060.36" m="173.534" cg="245.5"/>\r
+<eng-data t="1.972" f="1021.09" m="158.438" cg="245.5"/>\r
+<eng-data t="2.034" f="906.074" m="129.551" cg="245.5"/>\r
+<eng-data t="2.07" f="813.503" m="114.585" cg="245.5"/>\r
+<eng-data t="2.12" f="701.296" m="96.2741" cg="245.5"/>\r
+<eng-data t="2.162" f="633.972" m="82.7159" cg="245.5"/>\r
+<eng-data t="2.195" f="594.699" m="72.9134" cg="245.5"/>\r
+<eng-data t="2.246" f="530.18" m="59.0439" cg="245.5"/>\r
+<eng-data t="2.298" f="451.635" m="46.701" cg="245.5"/>\r
+<eng-data t="2.34" f="395.531" m="38.0989" cg="245.5"/>\r
+<eng-data t="2.407" f="328.207" m="26.3759" cg="245.5"/>\r
+<eng-data t="2.454" f="272.103" m="19.5547" cg="245.5"/>\r
+<eng-data t="2.53" f="210.389" m="10.6895" cg="245.5"/>\r
+<eng-data t="2.56" f="187.947" m="7.80046" cg="245.5"/>\r
+<eng-data t="2.602" f="162.701" m="4.24001" cg="245.5"/>\r
+<eng-data t="2.649" f="115.013" m="1.08442" cg="245.5"/>\r
+<eng-data t="2.688" f="0." m="0." cg="245.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+L990-BS 54 649 0 1.417 2.236 CTI \r
+0.01 800\r
+0.012 1450\r
+0.02 1625\r
+0.05 1320\r
+0.15 1230\r
+1.8 1150\r
+1.88 1105\r
+2 845\r
+2.203 825\r
+2.41 355\r
+2.6 320\r
+2.9 0\r
--- /dev/null
+L995-RL 75 486 0 1.996 3.591 CTI \r
+0.02 50\r
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+3.8 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+<eng-data t="7.23" f="0." m="0." cg="274."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; Pro75-4G 5506M1230-IM P\r
+M1230-IM 75 621 P 2.992 4.844 CTI\r
+ 0.117 270.318\r
+ 0.144 912.788\r
+ 0.212 1296.047\r
+ 0.408 1444.167\r
+ 1.087 1497.861\r
+ 1.767 1507.118\r
+ 2.403 1434.91\r
+ 2.949 1314.562\r
+ 3.352 1209.027\r
+ 3.648 1118.304\r
+ 3.909 868.352\r
+ 4.409 201.813\r
+ 4.586 111.09\r
+ 4.67 79.614\r
+ 4.7 0.0\r
--- /dev/null
+; Pro75-5G 6438M1300-IM/DT P\r
+M1300-IM 75 757 P 3.595 5.657 CTI\r
+ 0.0090 394.105\r
+ 0.057 934.778\r
+ 0.086 2146.406\r
+ 0.154 2615.423\r
+ 0.314 2827.132\r
+ 0.671 2758.734\r
+ 0.97 2752.22\r
+ 1.082 1172.543\r
+ 1.187 1120.43\r
+ 2.14 1172.543\r
+ 2.7 1139.973\r
+ 3.884 915.235\r
+ 4.372 771.924\r
+ 4.6 400.619\r
+ 4.697 335.478\r
+ 4.9 120.511\r
+ 4.901 0.0\r
+++ /dev/null
-;\r
-; Cesaroni Pro75 6251M1400\r
-; 'Classic Propellant'\r
-;\r
-; RockSim file by Kathy Miller\r
-; wRasp Adaptation by Len Lekx\r
-;\r
-M1400 75 7570 0 2.99 5.30 CTI\r
-0.10 1993.60 \r
-0.50 1891.25 \r
-1.10 1780.00 \r
-1.50 1691.00 \r
-2.00 1602.00 \r
-2.30 1557.50 \r
-2.50 1513.00 \r
-3.00 1335.00 \r
-3.50 1223.75 \r
-3.70 1112.00 \r
-3.90 667.50 \r
-4.00 534.00 \r
-4.40 222.50 \r
-4.47 0.00 \r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="M1450-Classic" Type="reloadable" dia="98."\r
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+<eng-data t="6.87" f="0." m="0." cg="351."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; Pro98-3G 7579M1520-BS P\r
+M1520-BS 98 548 P 3.737 6.718 CTI\r
+ 0.04 1427.795\r
+ 0.082 1706.389\r
+ 0.176 1620.489\r
+ 0.748 1734.249\r
+ 1.652 1827.113\r
+ 2.676 1715.676\r
+ 3.89 1423.152\r
+ 4.399 1404.579\r
+ 4.616 661.661\r
+ 4.877 69.649\r
+ 4.897 0.0\r
--- /dev/null
+M1540-IM 75 757 0 3.778 5.906 CTI \r
+0.02 800\r
+0.04 1250\r
+0.06 1800\r
+0.08 2400\r
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+0.35 2100\r
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+0.7 1900\r
+1.7 1830\r
+2.5 1720\r
+3.38 1550\r
+3.83 680\r
+4 530\r
+4.5 0\r
--- /dev/null
+; Pro98-2G 5342M1560-WT P\r
+M1560-WT 98 394 P 2.583 4.977 CTI\r
+ 0.037 1474.119\r
+ 0.121 1436.502\r
+ 0.328 1523.492\r
+ 1.299 1775.056\r
+ 1.545 1807.971\r
+ 1.797 1807.971\r
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+ 2.208 1737.439\r
+ 2.462 1572.864\r
+ 2.782 1415.343\r
+ 3.086 1309.545\r
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+ 3.258 1309.545\r
+ 3.328 679.459\r
+ 3.383 173.979\r
+ 3.428 68.181\r
+ 3.5 0.0\r
--- /dev/null
+; Pro75-6G 7545M1590-CL P\r
+M1590-CL 75 893 P 3.1590000000000003 5.223 CTI\r
+ 0.028 1210.592\r
+ 0.059 2024.222\r
+ 0.163 2235.371\r
+ 0.214 2302.939\r
+ 0.492 2153.727\r
+ 0.767 2091.79\r
+ 1.015 2103.051\r
+ 1.335 2083.344\r
+ 1.571 2029.852\r
+ 2.366 1779.288\r
+ 3.488 1534.354\r
+ 3.755 1030.41\r
+ 3.895 960.027\r
+ 4.12 650.341\r
+ 4.207 591.219\r
+ 4.44 340.655\r
+ 4.665 199.888\r
+ 4.778 90.091\r
+ 4.8 0.0\r
--- /dev/null
+; AMW75-7600 8212M1630-TT/DT P\r
+M1630-TT 75 1039 P 4.349 7.237 CTI\r
+ 0.0030 147.481\r
+ 0.032 2040.948\r
+ 0.078 3235.069\r
+ 0.158 3368.278\r
+ 0.463 3258.856\r
+ 0.647 2992.439\r
+ 0.949 2697.477\r
+ 1.052 2040.948\r
+ 1.101 1883.952\r
+ 1.392 1907.739\r
+ 1.786 1812.59\r
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+ 3.899 875.372\r
+ 4.595 347.294\r
+ 4.857 195.056\r
+ 4.891 166.511\r
+ 4.9 0.0\r
--- /dev/null
+M1670-BS 75 757 0 3.101 5.231 CTI \r
+0.055 100\r
+0.092 1500\r
+0.1 2000\r
+0.15 2200\r
+0.2 1800\r
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+1 2034\r
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+2 1900\r
+2.5 1760\r
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+3 1650\r
+3.3 530\r
+3.4 350\r
+3.9 0\r
--- /dev/null
+; Pro75-5G 6162M1675-PK P\r
+M1675-PK 75 757 P 3.1590000000000003 5.223 CTI\r
+ 0.04 1350.521\r
+ 0.077 1718.845\r
+ 0.166 1877.036\r
+ 0.307 2011.615\r
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+ 3.409 377.768\r
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+ 3.577 259.716\r
+ 3.69 113.33\r
+ 3.796 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
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--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; Pro98-4G 8088M1790-SK P\r
+M1790-SK 98 702 P 4.817 8.298 CTI\r
+ 0.059 1791.514\r
+ 0.199 1596.375\r
+ 0.6 1782.109\r
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+ 4.541 91.692\r
+ 4.597 0.0\r
--- /dev/null
+; Pro98-4G 9870M1800-BS P\r
+M1800-BS 98 702 P 4.9590000000000005 8.342 CTI\r
+ 0.02 1873.084\r
+ 0.059 2177.212\r
+ 0.265 1932.773\r
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+ 5.6 0.0\r
--- /dev/null
+M1810-RL 75 757 0 3.297 5.416 CTI \r
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+0.35 1915\r
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--- /dev/null
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--- /dev/null
+; Pro75-6G 7388-M2045-BS P\r
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--- /dev/null
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--- /dev/null
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--- /dev/null
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--- /dev/null
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--- /dev/null
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--- /dev/null
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--- /dev/null
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--- /dev/null
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--- /dev/null
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+++ /dev/null
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--- /dev/null
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+++ /dev/null
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--- /dev/null
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+</engine>\r
+</engine-list>\r
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--- /dev/null
+; Pro98 6G 10347 N10000-VM P\r
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+++ /dev/null
-;\r
-;\r
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--- /dev/null
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+ <engine-list>\r
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+<comments>N1100 Data Entered by Tim Van Milligan based on RMS case weight.\r
+Based on CAR certification data\r
+This data has not been approved by Cesaroni or Canadian Association of Rocketry.\r
+</comments>\r
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+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; Pro98 6G 14272 N1975-GR P\r
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--- /dev/null
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--- /dev/null
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--- /dev/null
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--- /dev/null
+; Pro98-6GXL 17613N2900-CL P\r
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--- /dev/null
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+ </engine>\r
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--- /dev/null
+; Pro98-6GXL 14263N3400-SK P\r
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--- /dev/null
+; Pro98-6GXL 17631N3800-BS P\r
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--- /dev/null
+; Pro98-6GXL 17790N4100-RL P\r
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--- /dev/null
+; Pro98-6GXL 20146N5800-CS P\r
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--- /dev/null
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+++ /dev/null
-;\r
-;Cesaroni Technologies Inc Motor Data File\r
-;Composed by Carl Tulanko for 150mm "O" CAR Certed Motor\r
-;24-Jun-2003 using CTI Cert graph to chart points\r
-O5100 150 803 1000 13.245 23.577 Cesaroni\r
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-5.9 0\r
--- /dev/null
+<engine-database>\r
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+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments><![CDATA[Cesaroni Technologies Inc Motor Data File\r
+Composed by Carl Tulanko for 150mm "O" CAR Certed Motor\r
+24-Jun-2003 using CTI Cert graph to chart points\r
+]]></comments>\r
+<data>\r
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+<eng-data t="5.32" f="1537.53" m="276.65" cg="401.5"/>\r
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+<eng-data t="5.89" f="333.44" m="-2.20114" cg="401.5"/>\r
+<eng-data t="5.86" f="0." m="0." cg="401.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Pro 150 O5800 White Thunder\r
-O5800 150 754 P 13.950000000000001 26.368000000000002 CTI\r
- 0.069 6337.621\r
- 0.103 5700.965\r
- 0.218 5874.598\r
- 0.378 6135.048\r
- 0.561 6337.621\r
- 0.745 6221.865\r
- 0.985 6221.865\r
- 1.18 6192.926\r
- 1.455 6308.682\r
- 1.753 6366.559\r
- 1.994 6337.621\r
- 2.269 6395.498\r
- 2.509 6308.682\r
- 2.83 6192.926\r
- 3.14 6048.232\r
- 3.426 5874.598\r
- 3.69 5729.904\r
- 3.965 5585.209\r
- 4.263 5382.637\r
- 4.572 5295.82\r
- 4.939 5180.064\r
- 5.053 5035.37\r
- 5.11 4717.042\r
- 5.133 4225.08\r
- 5.145 3675.241\r
- 5.156 3038.585\r
- 5.179 2344.051\r
- 5.214 1475.884\r
- 5.259 607.717\r
- 5.294 57.878\r
- 5.295 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="O5800" Type="reloadable" dia="161."\r
+len="754." initWt="26368." propWt="13950." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="5671.6" peakThrust="6320.61" throatDia="0."\r
+exitDia="0." Itot="30615.3" burn-time="5.4" massFrac="52.91" Isp="223.79"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve and engine data from C.A.R. web site.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="13950." cg="377."/>\r
+<eng-data t="0.05" f="5374.05" m="13888.8" cg="377."/>\r
+<eng-data t="0.056" f="5923.66" m="13873.3" cg="377."/>\r
+<eng-data t="0.112" f="5694.66" m="13725.1" cg="377."/>\r
+<eng-data t="0.149" f="5618.32" m="13629.7" cg="377."/>\r
+<eng-data t="0.186" f="5694.66" m="13534.4" cg="377."/>\r
+<eng-data t="0.267" f="5877.86" m="13320.8" cg="377."/>\r
+<eng-data t="0.385" f="6061.07" m="12999.9" cg="377."/>\r
+<eng-data t="0.497" f="6198.47" m="12687." cg="377."/>\r
+<eng-data t="0.578" f="6305.34" m="12456.3" cg="377."/>\r
+<eng-data t="0.658" f="6198.47" m="12228.4" cg="377."/>\r
+<eng-data t="0.752" f="6137.4" m="11964.2" cg="377."/>\r
+<eng-data t="0.907" f="6106.87" m="11531.8" cg="377."/>\r
+<eng-data t="1.099" f="6137.4" m="10996.2" cg="377."/>\r
+<eng-data t="1.342" f="6198.47" m="10313.3" cg="377."/>\r
+<eng-data t="1.547" f="6259.54" m="9731.44" cg="377."/>\r
+<eng-data t="1.807" f="6320.61" m="8986.26" cg="377."/>\r
+<eng-data t="2.087" f="6305.34" m="8180.83" cg="377."/>\r
+<eng-data t="2.28" f="6305.34" m="7626.33" cg="377."/>\r
+<eng-data t="2.553" f="6229.01" m="6846.73" cg="377."/>\r
+<eng-data t="2.894" f="6076.34" m="5890.74" cg="377."/>\r
+<eng-data t="3.242" f="5938.93" m="4938.12" cg="377."/>\r
+<eng-data t="3.578" f="5786.26" m="4040.56" cg="377."/>\r
+<eng-data t="3.981" f="5587.79" m="2996.26" cg="377."/>\r
+<eng-data t="4.248" f="5389.31" m="2328.53" cg="377."/>\r
+<eng-data t="4.553" f="5251.91" m="1589.1" cg="377."/>\r
+<eng-data t="4.845" f="5129.77" m="898.449" cg="377."/>\r
+<eng-data t="5.019" f="5022.9" m="495.978" cg="377."/>\r
+<eng-data t="5.118" f="4931.3" m="271.462" cg="377."/>\r
+<eng-data t="5.149" f="4717.56" m="203.316" cg="377."/>\r
+<eng-data t="5.18" f="4290.08" m="139.698" cg="377."/>\r
+<eng-data t="5.217" f="3541.99" m="73.6769" cg="377."/>\r
+<eng-data t="5.236" f="2732.82" m="46.515" cg="377."/>\r
+<eng-data t="5.248" f="1801.53" m="34.1184" cg="377."/>\r
+<eng-data t="5.286" f="946.565" m="10.327" cg="377."/>\r
+<eng-data t="5.298" f="381.679" m="6.69569" cg="377."/>\r
+<eng-data t="5.335" f="152.672" m="2.19132" cg="377."/>\r
+<eng-data t="5.398" f="0." m="0." cg="377."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Pro 150 O8000 White Thunder\r
-O8000 150 957 P 18.61 32.672000000000004 CTI\r
- 0.045 3964.63\r
- 0.046 6742.765\r
- 0.047 8623.794\r
- 0.125 7929.26\r
- 0.239 8160.772\r
- 0.364 8392.283\r
- 0.489 8508.039\r
- 0.614 8536.977\r
- 0.773 8392.283\r
- 0.989 8421.222\r
- 1.273 8479.1\r
- 1.602 8623.794\r
- 2.011 8565.916\r
- 2.33 8565.916\r
- 2.682 8479.1\r
- 3.102 8276.527\r
- 3.568 8045.016\r
- 3.886 7900.322\r
- 4.239 7668.81\r
- 4.591 7524.116\r
- 4.739 7524.116\r
- 4.909 7263.666\r
- 4.955 7003.215\r
- 4.977 6540.193\r
- 4.989 5845.659\r
- 5.0 5006.431\r
- 5.023 4051.447\r
- 5.034 3067.524\r
- 5.045 1996.785\r
- 5.08 1012.862\r
- 5.114 318.328\r
- 5.17 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Cesaroni Technology Inc." code="O8000" Type="reloadable" dia="161."\r
+len="597." initWt="32672." propWt="18610." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="7817.02" peakThrust="9389.31" throatDia="0."\r
+exitDia="0." Itot="41125.3" burn-time="5.26" massFrac="56.96" Isp="225.34"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve and engine data from C.A.R. web site.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="18610." cg="298.5"/>\r
+<eng-data t="0.056" f="9389.31" m="18491." cg="298.5"/>\r
+<eng-data t="0.075" f="8412.21" m="18414.5" cg="298.5"/>\r
+<eng-data t="0.099" f="8106.87" m="18324.8" cg="298.5"/>\r
+<eng-data t="0.124" f="7740.46" m="18235.2" cg="298.5"/>\r
+<eng-data t="0.199" f="7938.93" m="17969.1" cg="298.5"/>\r
+<eng-data t="0.304" f="8183.21" m="17586.1" cg="298.5"/>\r
+<eng-data t="0.41" f="8366.41" m="17189.2" cg="298.5"/>\r
+<eng-data t="0.491" f="8519.08" m="16879.7" cg="298.5"/>\r
+<eng-data t="0.547" f="8595.42" m="16662.8" cg="298.5"/>\r
+<eng-data t="0.602" f="8488.55" m="16450.2" cg="298.5"/>\r
+<eng-data t="0.671" f="8396.95" m="16186.6" cg="298.5"/>\r
+<eng-data t="0.789" f="8335.88" m="15739.9" cg="298.5"/>\r
+<eng-data t="0.913" f="8320.61" m="15272.6" cg="298.5"/>\r
+<eng-data t="1.019" f="8381.68" m="14872." cg="298.5"/>\r
+<eng-data t="1.248" f="8427.48" m="14001.1" cg="298.5"/>\r
+<eng-data t="1.547" f="8519.08" m="12854.6" cg="298.5"/>\r
+<eng-data t="1.901" f="8549.62" m="11487.5" cg="298.5"/>\r
+<eng-data t="2.161" f="8549.62" m="10481.6" cg="298.5"/>\r
+<eng-data t="2.441" f="8503.82" m="9401.17" cg="298.5"/>\r
+<eng-data t="2.714" f="8412.21" m="8356.29" cg="298.5"/>\r
+<eng-data t="2.963" f="8290.08" m="7415.3" cg="298.5"/>\r
+<eng-data t="3.286" f="8122.14" m="6215.87" cg="298.5"/>\r
+<eng-data t="3.59" f="7984.73" m="5107.99" cg="298.5"/>\r
+<eng-data t="3.851" f="7832.06" m="4173.95" cg="298.5"/>\r
+<eng-data t="4.075" f="7709.92" m="3386.25" cg="298.5"/>\r
+<eng-data t="4.28" f="7587.79" m="2676.69" cg="298.5"/>\r
+<eng-data t="4.484" f="7511.45" m="1979.76" cg="298.5"/>\r
+<eng-data t="4.652" f="7465.65" m="1410.45" cg="298.5"/>\r
+<eng-data t="4.77" f="7435.11" m="1012.62" cg="298.5"/>\r
+<eng-data t="4.851" f="7389.31" m="740.936" cg="298.5"/>\r
+<eng-data t="4.913" f="7297.71" m="534.905" cg="298.5"/>\r
+<eng-data t="4.969" f="7267.18" m="350.36" cg="298.5"/>\r
+<eng-data t="4.994" f="7145.04" m="268.838" cg="298.5"/>\r
+<eng-data t="5.075" f="3572.52" m="72.4169" cg="298.5"/>\r
+<eng-data t="5.13" f="1053.43" m="14.8502" cg="298.5"/>\r
+<eng-data t="5.161" f="305.344" m="5.3197" cg="298.5"/>\r
+<eng-data t="5.193" f="137.405" m="2.11407" cg="298.5"/>\r
+<eng-data t="5.261" f="0." m="0." cg="298.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-G100 38 406 0 0.093 0.511 Contrail_Rockets \r
-0 182.756\r
-0.199105 177.584\r
-0.606264 132.757\r
-0.986577 53.4476\r
-1.43 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="160.42" Itot="146.31" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="102.315" burn-time="1.43" cgDiv="10" cgFix="1" cgStep="-1." code="G100" delays="1000" dia="38." exitDia="0." initWt="511." len="406." mDiv="10" mFix="1" mStep="-1." massFrac="18.2" mfg="Contrail" peakThrust="182.756" propWt="93." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <data>\r
+ <eng-data cg="203." f="0." m="93." t="0."/>\r
+ <eng-data cg="203." f="182.756" m="93." t="0."/>\r
+ <eng-data cg="203." f="177.584" m="70.1979" t="0.199105"/>\r
+ <eng-data cg="203." f="132.757" m="30.0389" t="0.606264"/>\r
+ <eng-data cg="203." f="53.4476" m="7.53227" t="0.986577"/>\r
+ <eng-data cg="203." f="0." m="0." t="1.43"/>\r
+ </data>\r
+ </engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-G123 38 406 0 0.083 0.511 Contrail_Rockets \r
-0.00223714 217.239\r
-0.00671141 399.995\r
-0.0201342 220.687\r
-0.914989 72.4129\r
-0.955257 37.9306\r
-1.15 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="175.5" Itot="142.845" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="124.213" burn-time="1.15" cgDiv="10" cgFix="1" cgStep="-1." code="G123" delays="1000" dia="38." exitDia="0." initWt="511." len="406." mDiv="10" mFix="1" mStep="-1." massFrac="16.24" mfg="Contrail" peakThrust="399.995" propWt="83." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <data>\r
+ <eng-data cg="203." f="0." m="83." t="0."/>\r
+ <eng-data cg="203." f="217.239" m="82.8588" t="0.00223714"/>\r
+ <eng-data cg="203." f="399.995" m="82.0565" t="0.00671141"/>\r
+ <eng-data cg="203." f="220.687" m="79.636" t="0.0201342"/>\r
+ <eng-data cg="203." f="72.4129" m="3.43691" t="0.914989"/>\r
+ <eng-data cg="203." f="37.9306" m="2.14602" t="0.955257"/>\r
+ <eng-data cg="203." f="0." m="0." t="1.15"/>\r
+ </data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-G130 38 406 0 0.093 0.516 Contrail_Rockets \r
-0 662.061\r
-0.0145414 448.27\r
-0.0234899 241.376\r
-0.642058 41.3788\r
-0.86 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="113.07" Itot="103.119" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="119.906" burn-time="0.86" cgDiv="10" cgFix="1" cgStep="-1." code="G130" delays="1000" dia="38." exitDia="0." initWt="516." len="406." mDiv="10" mFix="1" mStep="-1." massFrac="18.02" mfg="Contrail" peakThrust="662.061" propWt="93." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+ <eng-data cg="203." f="0." m="93." t="0."/>\r
+ <eng-data cg="203." f="662.061" m="93." t="0."/>\r
+ <eng-data cg="203." f="448.27" m="85.7193" t="0.0145414"/>\r
+ <eng-data cg="203." f="241.376" m="82.9365" t="0.0234899"/>\r
+ <eng-data cg="203." f="41.3788" m="4.06661" t="0.642058"/>\r
+ <eng-data cg="203." f="0." m="0." t="0.86"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;G-234-HP Reload\r
-;38mm/16 Inch Hardware\r
-;Fast Nozzle\r
-G234 38 406.4 0 0.498 0.544 Contrail_Rockets \r
-0.00169492 245.419\r
-0.0973154 540.63\r
-0.183445 526.943\r
-0.202461 191.616\r
-0.237136 143.712\r
-0.260626 136.868\r
-0.533 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="24.23" Itot="118.345" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="222.035" burn-time="0.53" cgDiv="10" cgFix="1" cgStep="-1." code="G234" delays="1000" dia="38." exitDia="0." initWt="544." len="406.4" mDiv="10" mFix="1" mStep="-1." massFrac="91.54" mfg="Contrail" peakThrust="540.63" propWt="498." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>G-234-HP Reload\r
+38mm/16 Inch Hardware\r
+Fast Nozzle\r
+</comments>\r
+<data>\r
+<eng-data cg="203.2" f="0." m="498." t="0."/>\r
+<eng-data cg="203.2" f="245.419" m="497.125" t="0.00169492"/>\r
+<eng-data cg="203.2" f="540.63" m="338.982" t="0.0973154"/>\r
+<eng-data cg="203.2" f="526.943" m="145.518" t="0.183445"/>\r
+<eng-data cg="203.2" f="191.616" m="116.768" t="0.202461"/>\r
+<eng-data cg="203.2" f="143.712" m="92.3036" t="0.237136"/>\r
+<eng-data cg="203.2" f="136.868" m="78.4364" t="0.260626"/>\r
+<eng-data cg="203.2" f="0." m="0." t="0.533"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;G-300 PVC Motor for 38mm/16 Inch Case.\r
-;Motor uses Fast Nozzle\r
-;90cc's of Nitrous Oxide Used\r
-G300 38 406.4 0 0.023 0.544 Contrail_Rockets \r
-0.00111857 602.221\r
-0.0497763 814.367\r
-0.100671 670.655\r
-0.114094 266.893\r
-0.158837 239.52\r
-0.25 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="448.36" Itot="101.13" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="404.52" burn-time="0.25" cgDiv="10" cgFix="1" cgStep="-1." code="G300" delays="1000" dia="38." exitDia="0." initWt="544." len="406.4" mDiv="10" mFix="1" mStep="-1." massFrac="4.23" mfg="Contrail" peakThrust="814.367" propWt="23." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>G-300 PVC Motor for 38mm/16 Inch Case.\r
+Motor uses Fast Nozzle\r
+90cc's of Nitrous Oxide Used\r
+</comments>\r
+<data>\r
+<eng-data cg="203.2" f="0." m="23." t="0."/>\r
+<eng-data cg="203.2" f="602.221" m="22.9234" t="0.00111857"/>\r
+<eng-data cg="203.2" f="814.367" m="15.0852" t="0.0497763"/>\r
+<eng-data cg="203.2" f="670.655" m="6.49069" t="0.100671"/>\r
+<eng-data cg="203.2" f="266.893" m="5.05962" t="0.114094"/>\r
+<eng-data cg="203.2" f="239.52" m="2.48301" t="0.158837"/>\r
+<eng-data cg="203.2" f="0." m="0." t="0.25"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-H121 38 516 0 0.11 0.612 Contrail_Rockets \r
-0.00223714 251.721\r
-0.0402685 265.514\r
-0.0738255 203.446\r
-0.400447 179.308\r
-0.60179 134.481\r
-1.08949 127.585\r
-1.40268 93.1023\r
-1.61969 37.9306\r
-1.85 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="212.41" Itot="229.132" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="123.855" burn-time="1.85" cgDiv="10" cgFix="1" cgStep="-1." code="H121" delays="1000" dia="38." exitDia="0." initWt="612." len="516." mDiv="10" mFix="1" mStep="-1." massFrac="17.97" mfg="Contrail" peakThrust="265.514" propWt="110." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="258." f="0." m="110." t="0."/>\r
+<eng-data cg="258." f="251.721" m="109.865" t="0.00223714"/>\r
+<eng-data cg="258." f="265.514" m="105.143" t="0.0402685"/>\r
+<eng-data cg="258." f="203.446" m="101.366" t="0.0738255"/>\r
+<eng-data cg="258." f="179.308" m="71.3573" t="0.400447"/>\r
+<eng-data cg="258." f="134.481" m="56.192" t="0.60179"/>\r
+<eng-data cg="258." f="127.585" m="25.5131" t="1.08949"/>\r
+<eng-data cg="258." f="93.1023" m="8.92245" t="1.40268"/>\r
+<eng-data cg="258." f="37.9306" m="2.09691" t="1.61969"/>\r
+<eng-data cg="258." f="0." m="0." t="1.85"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-H141 38 516 0 0.125 0.612 Contrail_Rockets \r
-0.00223714 265.514\r
-0.111857 262.066\r
-1.20134 106.895\r
-1.25951 55.1717\r
-1.3557 27.5859\r
-1.7 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="198.76" Itot="243.645" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="143.32" burn-time="1.7" cgDiv="10" cgFix="1" cgStep="-1." code="H141" delays="1000" dia="38." exitDia="0." initWt="612." len="516." mDiv="10" mFix="1" mStep="-1." massFrac="20.42" mfg="Contrail" peakThrust="265.514" propWt="125." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="258." f="0." m="125." t="0."/>\r
+<eng-data cg="258." f="265.514" m="124.848" t="0.00223714"/>\r
+<eng-data cg="258." f="262.066" m="110.012" t="0.111857"/>\r
+<eng-data cg="258." f="106.895" m="6.89674" t="1.20134"/>\r
+<eng-data cg="258." f="55.1717" m="4.47841" t="1.25951"/>\r
+<eng-data cg="258." f="27.5859" m="2.43639" t="1.3557"/>\r
+<eng-data cg="258." f="0." m="0." t="1.7"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-H211 38 516 0 0.125 0.612 Contrail_Rockets \r
-0.00111857 531.028\r
-0.0190157 634.475\r
-0.0223714 593.096\r
-0.033557 544.821\r
-0.296421 317.238\r
-0.313199 186.205\r
-0.743848 96.5506\r
-0.97 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="170.07" Itot="208.478" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="214.925" burn-time="0.97" cgDiv="10" cgFix="1" cgStep="-1." code="H211" delays="1000" dia="38." exitDia="0." initWt="612." len="516." mDiv="10" mFix="1" mStep="-1." massFrac="20.42" mfg="Contrail" peakThrust="634.475" propWt="125." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="258." f="0." m="125." t="0."/>\r
+<eng-data cg="258." f="531.028" m="124.822" t="0.00111857"/>\r
+<eng-data cg="258." f="634.475" m="118.569" t="0.0190157"/>\r
+<eng-data cg="258." f="593.096" m="117.334" t="0.0223714"/>\r
+<eng-data cg="258." f="544.821" m="113.518" t="0.033557"/>\r
+<eng-data cg="258." f="317.238" m="45.5835" t="0.296421"/>\r
+<eng-data cg="258." f="186.205" m="43.0512" t="0.313199"/>\r
+<eng-data cg="258." f="96.5506" m="6.546" t="0.743848"/>\r
+<eng-data cg="258." f="0." m="0." t="0.97"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;H-222-HP Reload\r
-;38mm/16 inch Case Used\r
-;Medium Nozzle Used For Reload\r
-;140cc of Nitrous Oxide Used\r
-H222 38 406.4 0 0.022 0.52 Contrail_Rockets \r
-0 684.342\r
-0.0302013 656.968\r
-0.0525727 574.847\r
-0.0581655 349.014\r
-0.346756 260.05\r
-0.364653 191.616\r
-0.7 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="744.73" Itot="160.673" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="229.532" burn-time="0.7" cgDiv="10" cgFix="1" cgStep="-1." code="H222" delays="1000" dia="38." exitDia="0." initWt="520." len="406.4" mDiv="10" mFix="1" mStep="-1." massFrac="4.23" mfg="Contrail" peakThrust="684.342" propWt="22." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>H-222-HP Reload\r
+38mm/16 inch Case Used\r
+Medium Nozzle Used For Reload\r
+140cc of Nitrous Oxide Used\r
+</comments>\r
+<data>\r
+<eng-data cg="203.2" f="0." m="22." t="0."/>\r
+<eng-data cg="203.2" f="684.342" m="22." t="0."/>\r
+<eng-data cg="203.2" f="656.968" m="19.2266" t="0.0302013"/>\r
+<eng-data cg="203.2" f="574.847" m="17.34" t="0.0525727"/>\r
+<eng-data cg="203.2" f="349.014" m="16.9863" t="0.0581655"/>\r
+<eng-data cg="203.2" f="260.05" m="4.95265" t="0.346756"/>\r
+<eng-data cg="203.2" f="191.616" m="4.39924" t="0.364653"/>\r
+<eng-data cg="203.2" f="0." m="0." t="0.7"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;H-246 HP Reload\r
-;38mm/20 Inch Case Used\r
-;Medium Nozzle Used\r
-;185cc Nitrous Oxide Used\r
-H246 38 508 0 0.022 0.598 Contrail_Rockets \r
-0.00111857 609.064\r
-0.0123043 499.57\r
-0.502237 253.206\r
-0.514541 157.399\r
-0.9 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="1037.36" Itot="223.807" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="248.675" burn-time="0.9" cgDiv="10" cgFix="1" cgStep="-1." code="H246" delays="1000" dia="38." exitDia="0." initWt="598." len="508." mDiv="10" mFix="1" mStep="-1." massFrac="3.68" mfg="Contrail" peakThrust="609.064" propWt="22." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>H-246 HP Reload\r
+38mm/20 Inch Case Used\r
+Medium Nozzle Used\r
+185cc Nitrous Oxide Used\r
+</comments>\r
+<data>\r
+<eng-data cg="254." f="0." m="22." t="0."/>\r
+<eng-data cg="254." f="609.064" m="21.9665" t="0.00111857"/>\r
+<eng-data cg="254." f="499.57" m="21.357" t="0.0123043"/>\r
+<eng-data cg="254." f="253.206" m="3.23024" t="0.502237"/>\r
+<eng-data cg="254." f="157.399" m="2.98194" t="0.514541"/>\r
+<eng-data cg="254." f="0." m="0." t="0.9"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="766.94" Itot="263.24" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="239.309" burn-time="1.1" cgDiv="10" cgFix="1" cgStep="-1." code="H248" delays="1000" dia="38." exitDia="0." initWt="794." len="711.2" mDiv="10" mFix="1" mStep="-1." massFrac="4.41" mfg="Contrail" peakThrust="698.029" propWt="35." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>H-248-PVC Reload\r
+38mm/28 Inch Hardware\r
+Fast Nozzle\r
+</comments>\r
+<data>\r
+<eng-data cg="355.6" f="0." m="35." t="0."/>\r
+<eng-data cg="355.6" f="465.352" m="34.9308" t="0.00223714"/>\r
+<eng-data cg="355.6" f="698.029" m="28.702" t="0.082774"/>\r
+<eng-data cg="355.6" f="342.171" m="26.6909" t="0.111857"/>\r
+<eng-data cg="355.6" f="266.893" m="9.48034" t="0.536913"/>\r
+<eng-data cg="355.6" f="191.616" m="6.34358" t="0.639821"/>\r
+<eng-data cg="355.6" f="184.772" m="4.83218" t="0.700224"/>\r
+<eng-data cg="355.6" f="164.242" m="3.94977" t="0.738255"/>\r
+<eng-data cg="355.6" f="0." m="0." t="1.1"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-H277 38 719 0 0.11 0.71 Contrail_Rockets \r
-0 765.508\r
-0.0738255 703.44\r
-0.118568 337.927\r
-0.917226 179.308\r
-0.957494 75.8612\r
-0.995526 41.3788\r
-1.02908 48.2753\r
-1.15 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="274.26" Itot="295.856" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="257.266" burn-time="1.15" cgDiv="10" cgFix="1" cgStep="-1." code="H277" delays="1000" dia="38." exitDia="0." initWt="710." len="719." mDiv="10" mFix="1" mStep="-1." massFrac="15.49" mfg="Contrail" peakThrust="765.508" propWt="110." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="359.5" f="0." m="110." t="0."/>\r
+<eng-data cg="359.5" f="765.508" m="110." t="0."/>\r
+<eng-data cg="359.5" f="703.44" m="89.8398" t="0.0738255"/>\r
+<eng-data cg="359.5" f="337.927" m="81.1781" t="0.118568"/>\r
+<eng-data cg="359.5" f="179.308" m="4.3835" t="0.917226"/>\r
+<eng-data cg="359.5" f="75.8612" m="2.47333" t="0.957494"/>\r
+<eng-data cg="359.5" f="41.3788" m="1.64443" t="0.995526"/>\r
+<eng-data cg="359.5" f="48.2753" m="1.08519" t="1.02908"/>\r
+<eng-data cg="359.5" f="0." m="0." t="1.15"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-H300 38 516 0 0.11 0.612 Contrail_Rockets \r
-0 558.614\r
-0.115213 717.233\r
-0.12528 268.962\r
-0.214765 248.273\r
-0.286353 241.376\r
-0.334452 227.583\r
-0.62 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="151.01" Itot="162.901" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="262.744" burn-time="0.62" cgDiv="10" cgFix="1" cgStep="-1." code="H300" delays="1000" dia="38." exitDia="0." initWt="612." len="516." mDiv="10" mFix="1" mStep="-1." massFrac="17.97" mfg="Contrail" peakThrust="717.233" propWt="110." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="258." f="0." m="110." t="0."/>\r
+<eng-data cg="258." f="558.614" m="110." t="0."/>\r
+<eng-data cg="258." f="717.233" m="60.3706" t="0.115213"/>\r
+<eng-data cg="258." f="268.962" m="57.0187" t="0.12528"/>\r
+<eng-data cg="258." f="248.273" m="41.3916" t="0.214765"/>\r
+<eng-data cg="258." f="241.376" m="29.5567" t="0.286353"/>\r
+<eng-data cg="258." f="227.583" m="21.9411" t="0.334452"/>\r
+<eng-data cg="258." f="0." m="0." t="0.62"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;H-303-PVC Hybrid Motor\r
-;Uses Fast Nozzle\r
-;38mm/20 Inch Hardware\r
-;Uses 185cc Nitrous Oxide\r
-H303 38 508 0 0.023 0.589 Contrail_Rockets \r
-0 663.812\r
-0.0447427 780.15\r
-0.108501 704.872\r
-0.111857 342.171\r
-0.176734 328.484\r
-0.196868 307.954\r
-0.6 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="760.96" Itot="171.637" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="286.061" burn-time="0.6" cgDiv="10" cgFix="1" cgStep="-1." code="H303" delays="1000" dia="38." exitDia="0." initWt="589." len="508." mDiv="10" mFix="1" mStep="-1." massFrac="3.9" mfg="Contrail" peakThrust="780.15" propWt="23." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>H-303-PVC Hybrid Motor\r
+Uses Fast Nozzle\r
+38mm/20 Inch Hardware\r
+Uses 185cc Nitrous Oxide\r
+</comments>\r
+<data>\r
+<eng-data cg="254." f="0." m="23." t="0."/>\r
+<eng-data cg="254." f="663.812" m="23." t="0."/>\r
+<eng-data cg="254." f="780.15" m="18.6712" t="0.0447427"/>\r
+<eng-data cg="254." f="704.872" m="12.3273" t="0.108501"/>\r
+<eng-data cg="254." f="342.171" m="12.0919" t="0.111857"/>\r
+<eng-data cg="254." f="328.484" m="9.1766" t="0.176734"/>\r
+<eng-data cg="254." f="307.954" m="8.31804" t="0.196868"/>\r
+<eng-data cg="254." f="0." m="0." t="0.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-H340 38 711.2 0 0.024 0.816 Contrail_Rockets \r
-0 920.322\r
-0.0847458 715.806\r
-0.101695 345.121\r
-0.683051 332.338\r
-0.740678 255.645\r
-0.766102 153.387\r
-0.95 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="0." Itot="311.486" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="327.88" burn-time="0.95" cgDiv="10" cgFix="1" cgStep="-1." code="H340" delays="1000" dia="38." exitDia="0." initWt="816." len="711.2" mDiv="10" mFix="1" mStep="-1." massFrac="0." mfg="Contrail" peakThrust="920.322" propWt="24." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="0." f="0." m="0." t="0."/>\r
+<eng-data cg="0." f="920.322" m="0." t="0."/>\r
+<eng-data cg="0." f="715.806" m="0." t="0.0847458"/>\r
+<eng-data cg="0." f="345.121" m="0." t="0.101695"/>\r
+<eng-data cg="0." f="332.338" m="0." t="0.683051"/>\r
+<eng-data cg="0." f="255.645" m="0." t="0.740678"/>\r
+<eng-data cg="0." f="153.387" m="0." t="0.766102"/>\r
+<eng-data cg="0." f="0." m="0." t="0.95"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-I155 38 711.2 0 0.045 0.725 Contrail_Rockets \r
-0.0111857 222.411\r
-2.71253 150.555\r
-2.82998 82.121\r
-2.96421 58.1691\r
-3.5 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="1231.96" Itot="543.661" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="155.332" burn-time="3.5" cgDiv="10" cgFix="1" cgStep="-1." code="I155" delays="1000" dia="38." exitDia="0." initWt="725." len="711.2" mDiv="10" mFix="1" mStep="-1." massFrac="6.21" mfg="Contrail" peakThrust="222.411" propWt="45." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="355.6" f="0." m="45." t="0."/>\r
+<eng-data cg="355.6" f="222.411" m="44.897" t="0.0111857"/>\r
+<eng-data cg="355.6" f="150.555" m="3.20019" t="2.71253"/>\r
+<eng-data cg="355.6" f="82.121" m="2.0692" t="2.82998"/>\r
+<eng-data cg="355.6" f="58.1691" m="1.28986" t="2.96421"/>\r
+<eng-data cg="355.6" f="0." m="0." t="3.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-I210 38 922 0 0.125 0.87 Contrail_Rockets \r
-0 468.96\r
-0.464206 386.202\r
-0.497763 206.894\r
-2.25391 110.343\r
-2.34899 41.3788\r
-2.40492 13.7929\r
-2.72 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="406.19" Itot="497.923" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="183.06" burn-time="2.72" cgDiv="10" cgFix="1" cgStep="-1." code="I210" delays="1000" dia="38." exitDia="0." initWt="870." len="922." mDiv="10" mFix="1" mStep="-1." massFrac="14.37" mfg="Contrail" peakThrust="468.96" propWt="125." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="461." f="0." m="125." t="0."/>\r
+<eng-data cg="461." f="468.96" m="125." t="0."/>\r
+<eng-data cg="461." f="386.202" m="75.1716" t="0.464206"/>\r
+<eng-data cg="461." f="206.894" m="72.6734" t="0.497763"/>\r
+<eng-data cg="461." f="110.343" m="2.74356" t="2.25391"/>\r
+<eng-data cg="461." f="41.3788" m="0.932827" t="2.34899"/>\r
+<eng-data cg="461." f="13.7929" m="0.545499" t="2.40492"/>\r
+<eng-data cg="461." f="0." m="0." t="2.72"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-I221 38 719 0 0.125 0.71 Contrail_Rockets \r
-0 482.753\r
-0.503356 358.616\r
-0.519016 179.308\r
-1.49217 103.447\r
-1.53691 27.5859\r
-1.74 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="293.09" Itot="359.281" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="206.483" burn-time="1.74" cgDiv="10" cgFix="1" cgStep="-1." code="I221" delays="1000" dia="38." exitDia="0." initWt="710." len="719." mDiv="10" mFix="1" mStep="-1." massFrac="17.61" mfg="Contrail" peakThrust="482.753" propWt="125." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="359.5" f="0." m="125." t="0."/>\r
+<eng-data cg="359.5" f="482.753" m="125." t="0."/>\r
+<eng-data cg="359.5" f="358.616" m="51.327" t="0.503356"/>\r
+<eng-data cg="359.5" f="179.308" m="49.8616" t="0.519016"/>\r
+<eng-data cg="359.5" f="103.447" m="1.99441" t="1.49217"/>\r
+<eng-data cg="359.5" f="27.5859" m="0.97459" t="1.53691"/>\r
+<eng-data cg="359.5" f="0." m="0." t="1.74"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="666.3" Itot="431.257" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="253.681" burn-time="1.7" cgDiv="10" cgFix="1" cgStep="-1." code="I250" delays="1000" dia="38." exitDia="0." initWt="724." len="711.2" mDiv="10" mFix="1" mStep="-1." massFrac="9.12" mfg="Contrail" peakThrust="622.751" propWt="66." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>I-250-HP\r
+38mm/28 Inch Hardware\r
+430cc\r
+Medium Nozzle\r
+</comments>\r
+<data>\r
+<eng-data cg="355.6" f="0." m="66." t="0."/>\r
+<eng-data cg="355.6" f="622.751" m="65.7868" t="0.00447427"/>\r
+<eng-data cg="355.6" f="437.979" m="64.1525" t="0.0246085"/>\r
+<eng-data cg="355.6" f="273.737" m="10.7884" t="1.00447"/>\r
+<eng-data cg="355.6" f="171.085" m="10.1792" t="1.02237"/>\r
+<eng-data cg="355.6" f="157.399" m="5.68061" t="1.20134"/>\r
+<eng-data cg="355.6" f="136.868" m="4.82427" t="1.23937"/>\r
+<eng-data cg="355.6" f="0." m="0." t="1.7"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-I290 38 914.4 0 0.068 0.884 Contrail_Rockets \r
-0 521.516\r
-0.0847458 337.451\r
-0.138983 357.903\r
-0.19661 398.806\r
-0.308475 490.838\r
-0.40339 449.935\r
-0.589831 357.903\r
-0.762712 419.258\r
-0.932203 265.871\r
-1.08814 163.613\r
-1.24068 81.8064\r
-1.5 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="0." Itot="434.822" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="289.881" burn-time="1.5" cgDiv="10" cgFix="1" cgStep="-1." code="I290" delays="1000" dia="38." exitDia="0." initWt="884." len="914.4" mDiv="10" mFix="1" mStep="-1." massFrac="0." mfg="Contrail" peakThrust="521.516" propWt="68." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="0." f="0." m="0." t="0."/>\r
+<eng-data cg="0." f="521.516" m="0." t="0."/>\r
+<eng-data cg="0." f="337.451" m="0." t="0.0847458"/>\r
+<eng-data cg="0." f="357.903" m="0." t="0.138983"/>\r
+<eng-data cg="0." f="398.806" m="0." t="0.19661"/>\r
+<eng-data cg="0." f="490.838" m="0." t="0.308475"/>\r
+<eng-data cg="0." f="449.935" m="0." t="0.40339"/>\r
+<eng-data cg="0." f="357.903" m="0." t="0.589831"/>\r
+<eng-data cg="0." f="419.258" m="0." t="0.762712"/>\r
+<eng-data cg="0." f="265.871" m="0." t="0.932203"/>\r
+<eng-data cg="0." f="163.613" m="0." t="1.08814"/>\r
+<eng-data cg="0." f="81.8064" m="0." t="1.24068"/>\r
+<eng-data cg="0." f="0." m="0." t="1.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-I307 38 922 0 0.11 0.81 Contrail_Rockets \r
-0.00223714 551.717\r
-0.199105 717.233\r
-0.210291 386.202\r
-0.756152 620.682\r
-0.834452 455.167\r
-0.941834 310.341\r
-1.09172 199.998\r
-1.22371 117.24\r
-1.85 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="542.88" Itot="585.622" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="316.552" burn-time="1.85" cgDiv="10" cgFix="1" cgStep="-1." code="I307" delays="1000" dia="38." exitDia="0." initWt="810." len="922." mDiv="10" mFix="1" mStep="-1." massFrac="13.58" mfg="Contrail" peakThrust="717.233" propWt="110." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="461." f="0." m="110." t="0."/>\r
+<eng-data cg="461." f="551.717" m="109.884" t="0.00223714"/>\r
+<eng-data cg="461." f="717.233" m="86.4221" t="0.199105"/>\r
+<eng-data cg="461." f="386.202" m="85.2629" t="0.210291"/>\r
+<eng-data cg="461." f="620.682" m="33.6442" t="0.756152"/>\r
+<eng-data cg="461." f="455.167" m="25.7327" t="0.834452"/>\r
+<eng-data cg="461." f="310.341" m="18.0125" t="0.941834"/>\r
+<eng-data cg="461." f="199.998" m="10.8285" t="1.09172"/>\r
+<eng-data cg="461." f="117.24" m="6.89599" t="1.22371"/>\r
+<eng-data cg="461." f="0." m="0." t="1.85"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;I-333-PVC Reload\r
-;38mm/36 Inch Hardware\r
-;Uses Fast Nozzle\r
-;460cc Nitrous Oxide\r
-I333 38 914.4 0 0.068 0.929 Contrail_Rockets \r
-0.00894855 855.427\r
-0.0290828 881.09\r
-0.0536913 504.702\r
-0.604027 342.171\r
-0.796421 461.931\r
-1.7 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="835.93" Itot="557.44" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="327.906" burn-time="1.7" cgDiv="10" cgFix="1" cgStep="-1." code="I333" delays="1000" dia="38." exitDia="0." initWt="929." len="914.4" mDiv="10" mFix="1" mStep="-1." massFrac="7.32" mfg="Contrail" peakThrust="881.09" propWt="68." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>I-333-PVC Reload\r
+38mm/36 Inch Hardware\r
+Uses Fast Nozzle\r
+460cc Nitrous Oxide\r
+</comments>\r
+<data>\r
+<eng-data cg="457.2" f="0." m="68." t="0."/>\r
+<eng-data cg="457.2" f="855.427" m="67.5331" t="0.00894855"/>\r
+<eng-data cg="457.2" f="881.09" m="65.4006" t="0.0290828"/>\r
+<eng-data cg="457.2" f="504.702" m="63.3206" t="0.0536913"/>\r
+<eng-data cg="457.2" f="342.171" m="34.8939" t="0.604027"/>\r
+<eng-data cg="457.2" f="461.931" m="25.458" t="0.796421"/>\r
+<eng-data cg="457.2" f="0." m="0." t="1.7"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;I-400-HP\r
-;38mm/36 Inch Hardware\r
-;Uses Fast/X-Fast Nozzle\r
-;460cc Nitrous Oxide\r
-I400 38 914.4 0 0.086 0.925 Contrail_Rockets \r
-0.00447427 667.233\r
-0.0782998 898.199\r
-0.116331 598.799\r
-0.297539 521.811\r
-0.420582 410.605\r
-0.559284 487.594\r
-0.738255 367.834\r
-1 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="514.15" Itot="433.618" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="433.618" burn-time="1." cgDiv="10" cgFix="1" cgStep="-1." code="I400" delays="1000" dia="38." exitDia="0." initWt="925." len="914.4" mDiv="10" mFix="1" mStep="-1." massFrac="9.3" mfg="Contrail" peakThrust="898.199" propWt="86." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>I-400-HP\r
+38mm/36 Inch Hardware\r
+Uses Fast/X-Fast Nozzle\r
+460cc Nitrous Oxide\r
+</comments>\r
+<data>\r
+<eng-data cg="457.2" f="0." m="86." t="0."/>\r
+<eng-data cg="457.2" f="667.233" m="85.704" t="0.00447427"/>\r
+<eng-data cg="457.2" f="898.199" m="74.2435" t="0.0782998"/>\r
+<eng-data cg="457.2" f="598.799" m="68.5977" t="0.116331"/>\r
+<eng-data cg="457.2" f="521.811" m="48.4608" t="0.297539"/>\r
+<eng-data cg="457.2" f="410.605" m="37.0838" t="0.420582"/>\r
+<eng-data cg="457.2" f="487.594" m="24.7295" t="0.559284"/>\r
+<eng-data cg="457.2" f="367.834" m="9.54755" t="0.738255"/>\r
+<eng-data cg="457.2" f="0." m="0." t="1."/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-I500 38 719 0 0.748 0.8 Contrail_Rockets \r
-0.00111857 1155.16\r
-0.0201342 706.888\r
-0.0313199 999.988\r
-0.574944 103.447\r
-0.623043 120.688\r
-0.7 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="46.06" Itot="337.858" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="482.654" burn-time="0.7" cgDiv="10" cgFix="1" cgStep="-1." code="I500" delays="1000" dia="38." exitDia="0." initWt="800." len="719." mDiv="10" mFix="1" mStep="-1." massFrac="93.5" mfg="Contrail" peakThrust="1155.16" propWt="748." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="359.5" f="0." m="748." t="0."/>\r
+<eng-data cg="359.5" f="1155.16" m="746.57" t="0.00111857"/>\r
+<eng-data cg="359.5" f="706.888" m="707.374" t="0.0201342"/>\r
+<eng-data cg="359.5" f="999.988" m="686.239" t="0.0313199"/>\r
+<eng-data cg="359.5" f="103.447" m="22.2153" t="0.574944"/>\r
+<eng-data cg="359.5" f="120.688" m="10.2814" t="0.623043"/>\r
+<eng-data cg="359.5" f="0." m="0." t="0.7"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-I727 38 914.4 0 0.022 0.929 Contrail_Rockets \r
-0.00847458 1278.22\r
-0.0355932 1661.69\r
-0.0983051 1508.31\r
-0.144068 1482.74\r
-0.171186 1175.97\r
-0.218644 1022.58\r
-0.422034 792.499\r
-0.75 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="2854.63" Itot="615.877" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="821.169" burn-time="0.75" cgDiv="10" cgFix="1" cgStep="-1." code="I727" delays="1000" dia="38." exitDia="0." initWt="929." len="914.4" mDiv="10" mFix="1" mStep="-1." massFrac="2.37" mfg="Contrail" peakThrust="1661.69" propWt="22." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="457.2" f="0." m="22." t="0."/>\r
+<eng-data cg="457.2" f="1278.22" m="21.8065" t="0.00847458"/>\r
+<eng-data cg="457.2" f="1661.69" m="20.3826" t="0.0355932"/>\r
+<eng-data cg="457.2" f="1508.31" m="16.8319" t="0.0983051"/>\r
+<eng-data cg="457.2" f="1482.74" m="14.3872" t="0.144068"/>\r
+<eng-data cg="457.2" f="1175.97" m="13.0994" t="0.171186"/>\r
+<eng-data cg="457.2" f="1022.58" m="11.2358" t="0.218644"/>\r
+<eng-data cg="457.2" f="792.499" m="4.64223" t="0.422034"/>\r
+<eng-data cg="457.2" f="0." m="0." t="0.75"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-I747 38 711.2 0 0.068 0.839 Contrail_Rockets \r
-0 1917.34\r
-0.45 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="646.92" Itot="431.401" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="958.669" burn-time="0.45" cgDiv="10" cgFix="1" cgStep="-1." code="I747" delays="1000" dia="38." exitDia="0." initWt="839." len="711.2" mDiv="10" mFix="1" mStep="-1." massFrac="8.1" mfg="Contrail" peakThrust="1917.34" propWt="68." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="355.6" f="0." m="68." t="0."/>\r
+<eng-data cg="355.6" f="1917.34" m="68." t="0."/>\r
+<eng-data cg="355.6" f="0." m="0." t="0.45"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;J-150-HP\r
-;38mm/36 Inch\r
-;550cc\r
-;Slow Nozzle\r
-J150 38 914.4 0 0.091 0.839 Contrail_Rockets \r
-0 266.893\r
-2.00224 184.772\r
-2.75727 150.555\r
-3.00895 92.3861\r
-4.1 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="739.27" Itot="659.732" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="160.91" burn-time="4.1" cgDiv="10" cgFix="1" cgStep="-1." code="J150" delays="1000" dia="38." exitDia="0." initWt="839." len="914.4" mDiv="10" mFix="1" mStep="-1." massFrac="10.85" mfg="Contrail" peakThrust="266.893" propWt="91." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>J-150-HP\r
+38mm/36 Inch\r
+550cc\r
+Slow Nozzle\r
+</comments>\r
+<data>\r
+<eng-data cg="457.2" f="0." m="91." t="0."/>\r
+<eng-data cg="457.2" f="266.893" m="91." t="0."/>\r
+<eng-data cg="457.2" f="184.772" m="28.6299" t="2.00224"/>\r
+<eng-data cg="457.2" f="150.555" m="11.1687" t="2.75727"/>\r
+<eng-data cg="457.2" f="92.3861" m="6.95176" t="3.00895"/>\r
+<eng-data cg="457.2" f="0." m="0." t="4.1"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;J-222-HP Reload\r
-;Medium Nozzle\r
-;38mm/48 Inch Hardware\r
-;830cc\r
-J222 38 1219.2 0 0.091 1.043 Contrail_Rockets \r
-0.00559284 547.473\r
-0.167785 355.858\r
-2.86353 191.616\r
-2.95861 143.712\r
-3.08725 130.025\r
-3.46756 95.8079\r
-4.3 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="1041.1" Itot="929.081" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="216.065" burn-time="4.3" cgDiv="10" cgFix="1" cgStep="-1." code="J222" delays="1000" dia="38." exitDia="0." initWt="1043." len="1219.2" mDiv="10" mFix="1" mStep="-1." massFrac="8.72" mfg="Contrail" peakThrust="547.473" propWt="91." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>J-222-HP Reload\r
+Medium Nozzle\r
+38mm/48 Inch Hardware\r
+830cc\r
+</comments>\r
+<data>\r
+<eng-data cg="609.6" f="0." m="91." t="0."/>\r
+<eng-data cg="609.6" f="547.473" m="90.85" t="0.00559284"/>\r
+<eng-data cg="609.6" f="355.858" m="83.6748" t="0.167785"/>\r
+<eng-data cg="609.6" f="191.616" m="11.3979" t="2.86353"/>\r
+<eng-data cg="609.6" f="143.712" m="9.83646" t="2.95861"/>\r
+<eng-data cg="609.6" f="130.025" m="8.11195" t="3.08725"/>\r
+<eng-data cg="609.6" f="95.8079" m="3.90582" t="3.46756"/>\r
+<eng-data cg="609.6" f="0." m="0." t="4.3"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;J-234-BG Reload\r
-;Slow Nozzle\r
-;54mm/36 Inch Hardware\r
-J234 54 914.4 0 0.177 1.764 Contrail_Rockets \r
-0.00559284 229.255\r
-0.503356 349.014\r
-3.47875 208.724\r
-3.62416 116.338\r
-3.75839 78.6993\r
-4.3 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="594.74" Itot="1032.34" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="240.08" burn-time="4.3" cgDiv="10" cgFix="1" cgStep="-1." code="J234" delays="1000" dia="54." exitDia="0." initWt="1764." len="914.4" mDiv="10" mFix="1" mStep="-1." massFrac="10.03" mfg="Contrail" peakThrust="349.014" propWt="177." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>J-234-BG Reload\r
+Slow Nozzle\r
+54mm/36 Inch Hardware\r
+</comments>\r
+<data>\r
+<eng-data cg="457.2" f="0." m="177." t="0."/>\r
+<eng-data cg="457.2" f="229.255" m="176.89" t="0.00559284"/>\r
+<eng-data cg="457.2" f="349.014" m="152.214" t="0.503356"/>\r
+<eng-data cg="457.2" f="208.724" m="9.9505" t="3.47875"/>\r
+<eng-data cg="457.2" f="116.338" m="5.8984" t="3.62416"/>\r
+<eng-data cg="457.2" f="78.6993" m="3.65407" t="3.75839"/>\r
+<eng-data cg="457.2" f="0." m="0." t="4.3"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="704.4" Itot="759.862" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="245.117" burn-time="3.1" cgDiv="10" cgFix="1" cgStep="-1." code="J242 (38)" delays="1000" dia="38." exitDia="0." initWt="1065." len="1227." mDiv="10" mFix="1" mStep="-1." massFrac="10.33" mfg="Contrail" peakThrust="448.27" propWt="110." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="613.5" f="0." m="110." t="0."/>\r
+<eng-data cg="613.5" f="448.27" m="109.637" t="0.0111857"/>\r
+<eng-data cg="613.5" f="268.962" m="19.9195" t="1.73937"/>\r
+<eng-data cg="613.5" f="165.515" m="19.216" t="1.76174"/>\r
+<eng-data cg="613.5" f="48.2753" m="0.435417" t="2.97539"/>\r
+<eng-data cg="613.5" f="0." m="0." t="3.1"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;J-245-BG Reload\r
-;Slow Nozzle\r
-;54mm/28 Inch Hardware\r
-J245 54 711.2 0 0.1 1.55 Contrail_Rockets \r
-0 444.822\r
-0.139821 355.858\r
-1.05145 307.954\r
-2.06376 184.772\r
-2.15884 102.651\r
-2.28188 68.4342\r
-2.62 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="656.4" Itot="643.706" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="245.689" burn-time="2.62" cgDiv="10" cgFix="1" cgStep="-1." code="J245" delays="1000" dia="54." exitDia="0." initWt="1550." len="711.2" mDiv="10" mFix="1" mStep="-1." massFrac="6.45" mfg="Contrail" peakThrust="444.822" propWt="100." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>J-245-BG Reload\r
+Slow Nozzle\r
+54mm/28 Inch Hardware\r
+</comments>\r
+<data>\r
+<eng-data cg="355.6" f="0." m="100." t="0."/>\r
+<eng-data cg="355.6" f="444.822" m="100." t="0."/>\r
+<eng-data cg="355.6" f="355.858" m="91.3041" t="0.139821"/>\r
+<eng-data cg="355.6" f="307.954" m="44.2989" t="1.05145"/>\r
+<eng-data cg="355.6" f="184.772" m="5.55514" t="2.06376"/>\r
+<eng-data cg="355.6" f="102.651" m="3.43242" t="2.15884"/>\r
+<eng-data cg="355.6" f="68.4342" m="1.79733" t="2.28188"/>\r
+<eng-data cg="355.6" f="0." m="0." t="2.62"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;J-246-HP Reload\r
-;38mm/36 Inch Hardware\r
-;550cc\r
-;Medium Nozzle\r
-J246 38 914.4 0 0.068 0.861 Contrail_Rockets \r
-0.0167785 492.726\r
-0.0279642 328.484\r
-0.134228 526.943\r
-0.341163 403.762\r
-0.520134 349.014\r
-2.00224 191.616\r
-2.12528 116.338\r
-2.8 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="1014.72" Itot="676.666" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="241.666" burn-time="2.8" cgDiv="10" cgFix="1" cgStep="-1." code="J246" delays="1000" dia="38." exitDia="0." initWt="861." len="914.4" mDiv="10" mFix="1" mStep="-1." massFrac="7.9" mfg="Contrail" peakThrust="526.943" propWt="68." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>J-246-HP Reload\r
+38mm/36 Inch Hardware\r
+550cc\r
+Medium Nozzle\r
+</comments>\r
+<data>\r
+<eng-data cg="457.2" f="0." m="68." t="0."/>\r
+<eng-data cg="457.2" f="492.726" m="67.5846" t="0.0167785"/>\r
+<eng-data cg="457.2" f="328.484" m="67.123" t="0.0279642"/>\r
+<eng-data cg="457.2" f="526.943" m="62.5556" t="0.134228"/>\r
+<eng-data cg="457.2" f="403.762" m="52.8784" t="0.341163"/>\r
+<eng-data cg="457.2" f="349.014" m="46.1089" t="0.520134"/>\r
+<eng-data cg="457.2" f="191.616" m="5.84799" t="2.00224"/>\r
+<eng-data cg="457.2" f="116.338" m="3.94412" t="2.12528"/>\r
+<eng-data cg="457.2" f="0." m="0." t="2.8"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J272 54 914.4 0 0.114 1.746 Contrail_Rockets \r
-0.00847458 398.806\r
-0.169492 572.645\r
-0.533898 460.161\r
-0.872881 388.58\r
-1.05932 357.903\r
-2.91525 204.516\r
-3.19492 71.5806\r
-3.51695 40.9032\r
-3.63559 51.129\r
-3.86 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="958.3" Itot="1071.34" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="277.55" burn-time="3.86" cgDiv="10" cgFix="1" cgStep="-1." code="J272" delays="1000" dia="54." exitDia="0." initWt="1746." len="914.4" mDiv="10" mFix="1" mStep="-1." massFrac="6.53" mfg="Contrail" peakThrust="572.645" propWt="114." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="457.2" f="0." m="114." t="0."/>\r
+<eng-data cg="457.2" f="398.806" m="113.82" t="0.00847458"/>\r
+<eng-data cg="457.2" f="572.645" m="105.498" t="0.169492"/>\r
+<eng-data cg="457.2" f="460.161" m="85.4739" t="0.533898"/>\r
+<eng-data cg="457.2" f="388.58" m="70.1666" t="0.872881"/>\r
+<eng-data cg="457.2" f="357.903" m="62.7619" t="1.05932"/>\r
+<eng-data cg="457.2" f="204.516" m="7.22672" t="2.91525"/>\r
+<eng-data cg="457.2" f="71.5806" m="3.11864" t="3.19492"/>\r
+<eng-data cg="457.2" f="40.9032" m="1.19139" t="3.51695"/>\r
+<eng-data cg="457.2" f="51.129" m="0.610449" t="3.63559"/>\r
+<eng-data cg="457.2" f="0." m="0." t="3.86"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J292 54 711.2 0 0.136 1.542 Contrail_Rockets \r
-0.00847458 552.193\r
-0.262712 480.612\r
-0.423729 419.258\r
-0.762712 337.451\r
-1.97458 245.419\r
-2.07627 143.161\r
-2.53 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="554.66" Itot="739.748" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="292.391" burn-time="2.53" cgDiv="10" cgFix="1" cgStep="-1." code="J292" delays="1000" dia="54." exitDia="0." initWt="1542." len="711.2" mDiv="10" mFix="1" mStep="-1." massFrac="8.82" mfg="Contrail" peakThrust="552.193" propWt="136." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="355.6" f="0." m="136." t="0."/>\r
+<eng-data cg="355.6" f="552.193" m="135.57" t="0.00847458"/>\r
+<eng-data cg="355.6" f="480.612" m="111.433" t="0.262712"/>\r
+<eng-data cg="355.6" f="419.258" m="98.1137" t="0.423729"/>\r
+<eng-data cg="355.6" f="337.451" m="74.5343" t="0.762712"/>\r
+<eng-data cg="355.6" f="245.419" m="9.60349" t="1.97458"/>\r
+<eng-data cg="355.6" f="143.161" m="5.97099" t="2.07627"/>\r
+<eng-data cg="355.6" f="0." m="0." t="2.53"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J333 38 1227 0 0.11 1.064 Contrail_Rockets \r
-0 717.233\r
-0.204139 799.99\r
-0.752237 448.27\r
-0.763423 268.962\r
-2.16443 62.0682\r
-2.23714 27.5859\r
-2.4 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="684.46" Itot="738.352" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="307.646" burn-time="2.4" cgDiv="10" cgFix="1" cgStep="-1." code="J333" delays="1000" dia="38." exitDia="0." initWt="1064." len="1227." mDiv="10" mFix="1" mStep="-1." massFrac="10.34" mfg="Contrail" peakThrust="799.99" propWt="110." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="613.5" f="0." m="110." t="0."/>\r
+<eng-data cg="613.5" f="717.233" m="110." t="0."/>\r
+<eng-data cg="613.5" f="799.99" m="86.9286" t="0.204139"/>\r
+<eng-data cg="613.5" f="448.27" m="35.9646" t="0.752237"/>\r
+<eng-data cg="613.5" f="268.962" m="35.367" t="0.763423"/>\r
+<eng-data cg="613.5" f="62.0682" m="0.820241" t="2.16443"/>\r
+<eng-data cg="613.5" f="27.5859" m="0.334658" t="2.23714"/>\r
+<eng-data cg="613.5" f="0." m="0." t="2.4"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;J-345-PVC\r
-;38mm/48 Inch Hardware\r
-;735cc\r
-;Fast Nozzle\r
-J345 38 1219.2 0 0.098 1.118 Contrail_Rockets \r
-0.00559284 881.09\r
-0.0782998 667.233\r
-1.21924 376.388\r
-1.26398 359.279\r
-2.7 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="966.16" Itot="928.528" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="343.899" burn-time="2.7" cgDiv="10" cgFix="1" cgStep="-1." code="J345" delays="1000" dia="38." exitDia="0." initWt="1118." len="1219.2" mDiv="10" mFix="1" mStep="-1." massFrac="8.77" mfg="Contrail" peakThrust="881.09" propWt="98." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>J-345-PVC\r
+38mm/48 Inch Hardware\r
+735cc\r
+Fast Nozzle\r
+</comments>\r
+<data>\r
+<eng-data cg="609.6" f="0." m="98." t="0."/>\r
+<eng-data cg="609.6" f="881.09" m="97.74" t="0.00559284"/>\r
+<eng-data cg="609.6" f="667.233" m="91.7992" t="0.0782998"/>\r
+<eng-data cg="609.6" f="376.388" m="28.9635" t="1.21924"/>\r
+<eng-data cg="609.6" f="359.279" m="27.2266" t="1.26398"/>\r
+<eng-data cg="609.6" f="0." m="0." t="2.7"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J355 54 711.2 0 0.09 1.564 Contrail_Rockets \r
-0 562.419\r
-0.176271 501.064\r
-0.2 286.322\r
-0.433898 286.322\r
-0.688136 337.451\r
-0.701695 501.064\r
-0.80678 490.838\r
-1.00339 521.516\r
-1.21695 419.258\r
-1.31186 429.484\r
-1.37627 460.161\r
-1.49831 429.484\r
-1.54576 224.968\r
-1.64068 122.71\r
-1.91 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="769.18" Itot="678.879" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="355.434" burn-time="1.91" cgDiv="10" cgFix="1" cgStep="-1." code="J355" delays="1000" dia="54." exitDia="0." initWt="1564." len="711.2" mDiv="10" mFix="1" mStep="-1." massFrac="5.75" mfg="Contrail" peakThrust="562.419" propWt="90." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="355.6" f="0." m="90." t="0."/>\r
+<eng-data cg="355.6" f="562.419" m="90." t="0."/>\r
+<eng-data cg="355.6" f="501.064" m="77.574" t="0.176271"/>\r
+<eng-data cg="355.6" f="286.322" m="76.3355" t="0.2"/>\r
+<eng-data cg="355.6" f="286.322" m="67.4571" t="0.433898"/>\r
+<eng-data cg="355.6" f="337.451" m="56.9451" t="0.688136"/>\r
+<eng-data cg="355.6" f="501.064" m="56.1915" t="0.701695"/>\r
+<eng-data cg="355.6" f="490.838" m="49.2822" t="0.80678"/>\r
+<eng-data cg="355.6" f="521.516" m="36.0888" t="1.00339"/>\r
+<eng-data cg="355.6" f="419.258" m="22.7712" t="1.21695"/>\r
+<eng-data cg="355.6" f="429.484" m="17.4314" t="1.31186"/>\r
+<eng-data cg="355.6" f="460.161" m="13.6332" t="1.37627"/>\r
+<eng-data cg="355.6" f="429.484" m="6.43681" t="1.49831"/>\r
+<eng-data cg="355.6" f="224.968" m="4.37806" t="1.54576"/>\r
+<eng-data cg="355.6" f="122.71" m="2.19064" t="1.64068"/>\r
+<eng-data cg="355.6" f="0." m="0." t="1.91"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J358 54 914.4 0 0.111 1.743 Contrail_Rockets \r
-0.00847458 726.032\r
-0.0932203 726.032\r
-0.110169 501.064\r
-0.483051 480.612\r
-0.550847 398.806\r
-2.23729 286.322\r
-2.32203 153.387\r
-2.44915 112.484\r
-2.69 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="0." Itot="914.629" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="340.011" burn-time="2.69" cgDiv="10" cgFix="1" cgStep="-1." code="J358" delays="1000" dia="54." exitDia="0." initWt="1743." len="914.4" mDiv="10" mFix="1" mStep="-1." massFrac="0." mfg="Contrail" peakThrust="726.032" propWt="111." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="0." f="0." m="0." t="0."/>\r
+<eng-data cg="0." f="726.032" m="0." t="0.00847458"/>\r
+<eng-data cg="0." f="726.032" m="0." t="0.0932203"/>\r
+<eng-data cg="0." f="501.064" m="0." t="0.110169"/>\r
+<eng-data cg="0." f="480.612" m="0." t="0.483051"/>\r
+<eng-data cg="0." f="398.806" m="0." t="0.550847"/>\r
+<eng-data cg="0." f="286.322" m="0." t="2.23729"/>\r
+<eng-data cg="0." f="153.387" m="0." t="2.32203"/>\r
+<eng-data cg="0." f="112.484" m="0." t="2.44915"/>\r
+<eng-data cg="0." f="0." m="0." t="2.69"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J416 54 914.4 0 0.158 1.7 Contrail_Rockets \r
-0 787.386\r
-0.0762712 777.161\r
-0.211864 572.645\r
-0.432203 531.741\r
-0.864407 511.29\r
-1.26271 480.612\r
-1.82203 470.387\r
-2.00847 347.677\r
-2.13559 276.097\r
-2.24576 184.064\r
-2.40678 81.8064\r
-2.75 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="734.74" Itot="1138.44" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="413.979" burn-time="2.75" cgDiv="10" cgFix="1" cgStep="-1." code="J416" delays="1000" dia="54." exitDia="0." initWt="1700." len="914.4" mDiv="10" mFix="1" mStep="-1." massFrac="9.29" mfg="Contrail" peakThrust="787.386" propWt="158." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="457.2" f="0." m="158." t="0."/>\r
+<eng-data cg="457.2" f="787.386" m="158." t="0."/>\r
+<eng-data cg="457.2" f="777.161" m="149.719" t="0.0762712"/>\r
+<eng-data cg="457.2" f="572.645" m="137.019" t="0.211864"/>\r
+<eng-data cg="457.2" f="531.741" m="120.133" t="0.432203"/>\r
+<eng-data cg="457.2" f="511.29" m="88.8502" t="0.864407"/>\r
+<eng-data cg="457.2" f="480.612" m="61.4344" t="1.26271"/>\r
+<eng-data cg="457.2" f="470.387" m="24.5233" t="1.82203"/>\r
+<eng-data cg="457.2" f="347.677" m="13.9394" t="2.00847"/>\r
+<eng-data cg="457.2" f="276.097" m="8.43701" t="2.13559"/>\r
+<eng-data cg="457.2" f="184.064" m="4.91908" t="2.24576"/>\r
+<eng-data cg="457.2" f="81.8064" m="1.94839" t="2.40678"/>\r
+<eng-data cg="457.2" f="0." m="0." t="2.75"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J555 38 1227 0 0.166 1.132 Contrail_Rockets \r
-0 931.023\r
-0.0581655 1344.81\r
-0.277405 810.335\r
-1.17226 241.376\r
-1.2774 68.9647\r
-1.31767 51.7235\r
-1.6 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="490.84" Itot="799.045" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="499.403" burn-time="1.6" cgDiv="10" cgFix="1" cgStep="-1." code="J555" delays="1000" dia="38." exitDia="0." initWt="1132." len="1227." mDiv="10" mFix="1" mStep="-1." massFrac="14.66" mfg="Contrail" peakThrust="1344.81" propWt="166." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="613.5" f="0." m="166." t="0."/>\r
+<eng-data cg="613.5" f="931.023" m="166." t="0."/>\r
+<eng-data cg="613.5" f="1344.81" m="152.25" t="0.0581655"/>\r
+<eng-data cg="613.5" f="810.335" m="103.17" t="0.277405"/>\r
+<eng-data cg="613.5" f="241.376" m="5.41105" t="1.17226"/>\r
+<eng-data cg="613.5" f="68.9647" m="2.02172" t="1.2774"/>\r
+<eng-data cg="613.5" f="51.7235" m="1.51688" t="1.31767"/>\r
+<eng-data cg="613.5" f="0." m="0." t="1.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J642 54 914.4 0 0.159 1.791 Contrail_Rockets \r
-0.00677966 1482.74\r
-0.0779661 997.015\r
-0.471186 1303.79\r
-0.542373 818.064\r
-0.633898 741.37\r
-0.742373 587.983\r
-1.25085 485.725\r
-1.29831 332.338\r
-1.39661 178.951\r
-1.47458 51.129\r
-1.72 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="703.8" Itot="1097.4" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="638.024" burn-time="1.72" cgDiv="10" cgFix="1" cgStep="-1." code="J642" delays="1000" dia="54." exitDia="0." initWt="1791." len="914.4" mDiv="10" mFix="1" mStep="-1." massFrac="8.88" mfg="Contrail" peakThrust="1482.74" propWt="159." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="457.2" f="0." m="159." t="0."/>\r
+<eng-data cg="457.2" f="1482.74" m="158.272" t="0.00677966"/>\r
+<eng-data cg="457.2" f="997.015" m="145.484" t="0.0779661"/>\r
+<eng-data cg="457.2" f="1303.79" m="79.942" t="0.471186"/>\r
+<eng-data cg="457.2" f="818.064" m="68.9995" t="0.542373"/>\r
+<eng-data cg="457.2" f="741.37" m="58.6598" t="0.633898"/>\r
+<eng-data cg="457.2" f="587.983" m="48.2133" t="0.742373"/>\r
+<eng-data cg="457.2" f="485.725" m="8.66229" t="1.25085"/>\r
+<eng-data cg="457.2" f="332.338" m="5.84978" t="1.29831"/>\r
+<eng-data cg="457.2" f="178.951" m="2.20858" t="1.39661"/>\r
+<eng-data cg="457.2" f="51.129" m="0.909045" t="1.47458"/>\r
+<eng-data cg="457.2" f="0." m="0." t="1.72"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;J-800-HP\r
-;38mm/48 Inch\r
-;685cc\r
-;XXF Nozzle (Short Nozzle)\r
-J800 38 1219.2 0 0.105 1.148 Contrail_Rockets \r
-0.00223714 1830.61\r
-0.52349 889.644\r
-0.639821 650.125\r
-0.740492 444.822\r
-0.823266 273.737\r
-0.90604 153.977\r
-0.997763 136.868\r
-1.2 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="903.48" Itot="930.313" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="775.261" burn-time="1.2" cgDiv="10" cgFix="1" cgStep="-1." code="J800" delays="1000" dia="38." exitDia="0." initWt="1148." len="1219.2" mDiv="10" mFix="1" mStep="-1." massFrac="9.15" mfg="Contrail" peakThrust="1830.61" propWt="105." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>J-800-HP\r
+38mm/48 Inch\r
+685cc\r
+XXF Nozzle (Short Nozzle)\r
+</comments>\r
+<data>\r
+<eng-data cg="609.6" f="0." m="105." t="0."/>\r
+<eng-data cg="609.6" f="1830.61" m="104.769" t="0.00223714"/>\r
+<eng-data cg="609.6" f="889.644" m="24.7508" t="0.52349"/>\r
+<eng-data cg="609.6" f="650.125" m="14.6425" t="0.639821"/>\r
+<eng-data cg="609.6" f="444.822" m="8.42192" t="0.740492"/>\r
+<eng-data cg="609.6" f="273.737" m="5.06542" t="0.823266"/>\r
+<eng-data cg="609.6" f="153.977" m="3.0675" t="0.90604"/>\r
+<eng-data cg="609.6" f="136.868" m="1.56204" t="0.997763"/>\r
+<eng-data cg="609.6" f="0." m="0." t="1.2"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;K-234-BG Reload\r
-;Slow Nozzle\r
-;54mm/48 Inch Hardware\r
-K234 54 1219.2 0 0.385 2.063 Contrail_Rockets \r
-0 92.3861\r
-0.234899 396.918\r
-0.973154 338.749\r
-5.97315 171.085\r
-6.05145 106.073\r
-6.19687 78.6993\r
-6.37584 54.7473\r
-7.05 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="439.22" Itot="1658.29" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="235.218" burn-time="7.05" cgDiv="10" cgFix="1" cgStep="-1." code="K234" delays="1000" dia="54." exitDia="0." initWt="2063." len="1219.2" mDiv="10" mFix="1" mStep="-1." massFrac="18.66" mfg="Contrail" peakThrust="396.918" propWt="385." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>K-234-BG Reload\r
+Slow Nozzle\r
+54mm/48 Inch Hardware\r
+</comments>\r
+<data>\r
+<eng-data cg="609.6" f="0." m="385." t="0."/>\r
+<eng-data cg="609.6" f="92.3861" m="385." t="0."/>\r
+<eng-data cg="609.6" f="396.918" m="371.658" t="0.234899"/>\r
+<eng-data cg="609.6" f="338.749" m="308.612" t="0.973154"/>\r
+<eng-data cg="609.6" f="171.085" m="12.6952" t="5.97315"/>\r
+<eng-data cg="609.6" f="106.073" m="10.176" t="6.05145"/>\r
+<eng-data cg="609.6" f="78.6993" m="7.05688" t="6.19687"/>\r
+<eng-data cg="609.6" f="54.7473" m="4.28446" t="6.37584"/>\r
+<eng-data cg="609.6" f="0." m="0." t="7.05"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-K265 54 1219.2 0 0.271 2.085 Contrail_Rockets \r
-0 470.387\r
-2.44068 347.677\r
-3.91525 224.968\r
-4.77966 173.839\r
-5.13559 112.484\r
-5.33898 51.129\r
-6.26 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="633.66" Itot="1684.02" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="269.013" burn-time="6.26" cgDiv="10" cgFix="1" cgStep="-1." code="K265" delays="1000" dia="54." exitDia="0." initWt="2085." len="1219.2" mDiv="10" mFix="1" mStep="-1." massFrac="13." mfg="Contrail" peakThrust="470.387" propWt="271." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="609.6" f="0." m="271." t="0."/>\r
+<eng-data cg="609.6" f="470.387" m="271." t="0."/>\r
+<eng-data cg="609.6" f="347.677" m="110.347" t="2.44068"/>\r
+<eng-data cg="609.6" f="224.968" m="42.4043" t="3.91525"/>\r
+<eng-data cg="609.6" f="173.839" m="14.6666" t="4.77966"/>\r
+<eng-data cg="609.6" f="112.484" m="6.46656" t="5.13559"/>\r
+<eng-data cg="609.6" f="51.129" m="3.78901" t="5.33898"/>\r
+<eng-data cg="609.6" f="0." m="0." t="6.26"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;K-300-BS\r
-;75mm/40 Inch Hardware\r
-;2050cc\r
-;Slow Nozzle\r
-K300 75 1016 0 0.181 4.059 Contrail_Rockets \r
-0 431.135\r
-0.324385 526.943\r
-0.98434 479.039\r
-1.1745 369.545\r
-5 280.58\r
-5.19016 171.085\r
-5.35794 102.651\r
-5.6264 54.7473\r
-5.79418 27.3737\r
-6.5 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="1078.95" Itot="1915.14" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="294.637" burn-time="6.5" cgDiv="10" cgFix="1" cgStep="-1." code="K300" delays="1000" dia="75." exitDia="0." initWt="4059." len="1016." mDiv="10" mFix="1" mStep="-1." massFrac="4.46" mfg="Contrail" peakThrust="526.943" propWt="181." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>K-300-BS\r
+75mm/40 Inch Hardware\r
+2050cc\r
+Slow Nozzle\r
+</comments>\r
+<data>\r
+<eng-data cg="508." f="0." m="181." t="0."/>\r
+<eng-data cg="508." f="431.135" m="181." t="0."/>\r
+<eng-data cg="508." f="526.943" m="166.314" t="0.324385"/>\r
+<eng-data cg="508." f="479.039" m="134.941" t="0.98434"/>\r
+<eng-data cg="508." f="369.545" m="127.316" t="1.1745"/>\r
+<eng-data cg="508." f="280.58" m="9.78984" t="5."/>\r
+<eng-data cg="508." f="171.085" m="5.73117" t="5.19016"/>\r
+<eng-data cg="508." f="102.651" m="3.56087" t="5.35794"/>\r
+<eng-data cg="508." f="54.7473" m="1.5641" t="5.6264"/>\r
+<eng-data cg="508." f="27.3737" m="0.91301" t="5.79418"/>\r
+<eng-data cg="508." f="0." m="0." t="6.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;K-321-BG Reload\r
-;54mm/48 Inch Hardware\r
-;Medium Nozzle\r
-K321 54 1219.2 0 0.183 2.043 Contrail_Rockets \r
-0.00559284 218.989\r
-0.218121 410.605\r
-0.973154 718.559\r
-0.989933 732.246\r
-1.05705 444.822\r
-1.4877 403.762\r
-3.97092 232.676\r
-4.11633 88.9644\r
-4.23378 54.7473\r
-4.34564 54.7473\r
-4.9 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="875.68" Itot="1571.52" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="320.718" burn-time="4.9" cgDiv="10" cgFix="1" cgStep="-1." code="K321" delays="1000" dia="54." exitDia="0." initWt="2043." len="1219.2" mDiv="10" mFix="1" mStep="-1." massFrac="8.96" mfg="Contrail" peakThrust="732.246" propWt="183." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>K-321-BG Reload\r
+54mm/48 Inch Hardware\r
+Medium Nozzle\r
+</comments>\r
+<data>\r
+<eng-data cg="609.6" f="0." m="183." t="0."/>\r
+<eng-data cg="609.6" f="218.989" m="182.929" t="0.00559284"/>\r
+<eng-data cg="609.6" f="410.605" m="175.138" t="0.218121"/>\r
+<eng-data cg="609.6" f="718.559" m="125.499" t="0.973154"/>\r
+<eng-data cg="609.6" f="732.246" m="124.081" t="0.989933"/>\r
+<eng-data cg="609.6" f="444.822" m="119.482" t="1.05705"/>\r
+<eng-data cg="609.6" f="403.762" m="98.2041" t="1.4877"/>\r
+<eng-data cg="609.6" f="232.676" m="6.18609" t="3.97092"/>\r
+<eng-data cg="609.6" f="88.9644" m="3.46297" t="4.11633"/>\r
+<eng-data cg="609.6" f="54.7473" m="2.48021" t="4.23378"/>\r
+<eng-data cg="609.6" f="54.7473" m="1.76708" t="4.34564"/>\r
+<eng-data cg="609.6" f="0." m="0." t="4.9"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;K-404-Sparky\r
-;75mm/40 Inch Hardware\r
-;2050cc\r
-;Slow Nozzle\r
-K404 75 1016 0 0.318 4.15 Contrail_Rockets \r
-0.0111857 670.655\r
-4.63087 335.328\r
-4.80984 205.303\r
-4.9217 130.025\r
-5.0783 82.121\r
-5.26846 41.0605\r
-6.4 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="784.38" Itot="2446.1" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="382.203" burn-time="6.4" cgDiv="10" cgFix="1" cgStep="-1." code="K404" delays="1000" dia="75." exitDia="0." initWt="4150." len="1016." mDiv="10" mFix="1" mStep="-1." massFrac="7.66" mfg="Contrail" peakThrust="670.655" propWt="318." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>K-404-Sparky\r
+75mm/40 Inch Hardware\r
+2050cc\r
+Slow Nozzle\r
+</comments>\r
+<data>\r
+<eng-data cg="508." f="0." m="318." t="0."/>\r
+<eng-data cg="508." f="670.655" m="317.512" t="0.0111857"/>\r
+<eng-data cg="508." f="335.328" m="15.4297" t="4.63087"/>\r
+<eng-data cg="508." f="205.303" m="9.14035" t="4.80984"/>\r
+<eng-data cg="508." f="130.025" m="6.70216" t="4.9217"/>\r
+<eng-data cg="508." f="82.121" m="4.54268" t="5.0783"/>\r
+<eng-data cg="508." f="41.0605" m="3.02007" t="5.26846"/>\r
+<eng-data cg="508." f="0." m="0." t="6.4"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-K456 75 813 0 0.58 3.704 Contrail_Rockets \r
-0.00559284 681.026\r
-0.212528 896.541\r
-0.503356 775.853\r
-1.36465 577.579\r
-1.52685 525.856\r
-2.51119 370.685\r
-2.66779 129.309\r
-3.7 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="286.19" Itot="1627.8" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="439.945" burn-time="3.7" cgDiv="10" cgFix="1" cgStep="-1." code="K456" delays="1000" dia="75." exitDia="0." initWt="3704." len="813." mDiv="10" mFix="1" mStep="-1." massFrac="15.66" mfg="Contrail" peakThrust="896.541" propWt="580." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="406.5" f="0." m="580." t="0."/>\r
+<eng-data cg="406.5" f="681.026" m="579.321" t="0.00559284"/>\r
+<eng-data cg="406.5" f="896.541" m="521.162" t="0.212528"/>\r
+<eng-data cg="406.5" f="775.853" m="434.511" t="0.503356"/>\r
+<eng-data cg="406.5" f="577.579" m="226.836" t="1.36465"/>\r
+<eng-data cg="406.5" f="525.856" m="194.95" t="1.52685"/>\r
+<eng-data cg="406.5" f="370.685" m="37.7284" t="2.51119"/>\r
+<eng-data cg="406.5" f="129.309" m="23.779" t="2.66779"/>\r
+<eng-data cg="406.5" f="0." m="0." t="3.7"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="143.93" Itot="2117.26" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="588.128" burn-time="3.6" cgDiv="10" cgFix="1" cgStep="-1." code="K543" delays="1000" dia="75." exitDia="0." initWt="3600." len="787.4" mDiv="10" mFix="1" mStep="-1." massFrac="41.67" mfg="Contrail" peakThrust="900." propWt="1500." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Contrail Rockets Hybrid Rocket Motor (K543)\r
+75mm-1400cc Motor Hardware w/ Slow Injector Kit and Nozzle\r
+Black Smoke Reload\r
+Data Input By Tom R. Sanders of Contrail Rockets LLC\r
+</comments>\r
+<data>\r
+<eng-data cg="393.7" f="0." m="1500." t="0."/>\r
+<eng-data cg="393.7" f="900." m="1500." t="0."/>\r
+<eng-data cg="393.7" f="472.868" m="45.963" t="2.98992"/>\r
+<eng-data cg="393.7" f="108.527" m="18.2877" t="3.1243"/>\r
+<eng-data cg="393.7" f="0." m="0." t="3.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="1101.92" Itot="1685.76" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="554.527" burn-time="3.04" cgDiv="10" cgFix="1" cgStep="-1." code="K555" delays="1000" dia="54." exitDia="0." initWt="2038." len="1219.2" mDiv="10" mFix="1" mStep="-1." massFrac="7.65" mfg="Contrail" peakThrust="1385.79" propWt="156." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>K-555-BG Reload\r
+54mm/48 Inch Case\r
+XF Nozzle\r
+</comments>\r
+<data>\r
+<eng-data cg="609.6" f="0." m="156." t="0."/>\r
+<eng-data cg="609.6" f="769.885" m="154.207" t="0.0503356"/>\r
+<eng-data cg="609.6" f="889.644" m="132.305" t="0.33557"/>\r
+<eng-data cg="609.6" f="1385.79" m="108.751" t="0.559284"/>\r
+<eng-data cg="609.6" f="872.536" m="78.9464" t="0.844519"/>\r
+<eng-data cg="609.6" f="581.691" m="67.6569" t="1.0123"/>\r
+<eng-data cg="609.6" f="342.171" m="4.54053" t="2.48881"/>\r
+<eng-data cg="609.6" f="222.411" m="2.49509" t="2.56711"/>\r
+<eng-data cg="609.6" f="136.868" m="1.28637" t="2.63982"/>\r
+<eng-data cg="609.6" f="51.3256" m="0.409769" t="2.74049"/>\r
+<eng-data cg="609.6" f="17.1085" m="0.179537" t="2.8132"/>\r
+<eng-data cg="609.6" f="0." m="0." t="3.04"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;K-630-Sparky Reload\r
-;75mm/41 Inch Hardare\r
-;1400cc\r
-;Medium Nozzle\r
-K630 75 1041.4 0 0.075 3.55 Contrail_Rockets \r
-0.00559284 307.954\r
-0.0978747 573.136\r
-0.500559 889.644\r
-1.75336 667.233\r
-1.85403 410.605\r
-1.93792 239.52\r
-2.04978 128.314\r
-2.2 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="1934.74" Itot="1423." Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="646.817" burn-time="2.2" cgDiv="10" cgFix="1" cgStep="-1." code="K630" delays="1000" dia="75." exitDia="0." initWt="3550." len="1041.4" mDiv="10" mFix="1" mStep="-1." massFrac="2.11" mfg="Contrail" peakThrust="889.644" propWt="75." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>K-630-Sparky Reload\r
+75mm/41 Inch Hardare\r
+1400cc\r
+Medium Nozzle\r
+</comments>\r
+<data>\r
+<eng-data cg="520.7" f="0." m="75." t="0."/>\r
+<eng-data cg="520.7" f="307.954" m="74.9546" t="0.00559284"/>\r
+<eng-data cg="520.7" f="573.136" m="72.8119" t="0.0978747"/>\r
+<eng-data cg="520.7" f="889.644" m="57.2891" t="0.500559"/>\r
+<eng-data cg="520.7" f="667.233" m="5.88897" t="1.75336"/>\r
+<eng-data cg="520.7" f="410.605" m="3.02953" t="1.85403"/>\r
+<eng-data cg="520.7" f="239.52" m="1.59227" t="1.93792"/>\r
+<eng-data cg="520.7" f="128.314" m="0.50796" t="2.04978"/>\r
+<eng-data cg="520.7" f="0." m="0." t="2.2"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;K-678-Sparky\r
-;75mm/40 Inch Hardware\r
-;2050cc\r
-;Medium Nozzle\r
-K678 75 1016 0 0.827 4.05 Contrail_Rockets \r
-0.00559284 1163.38\r
-2.21477 444.822\r
-2.32103 256.628\r
-2.38814 102.651\r
-2.8 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="228.12" Itot="1850.12" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="660.756" burn-time="2.8" cgDiv="10" cgFix="1" cgStep="-1." code="K678" delays="1000" dia="75." exitDia="0." initWt="4050." len="1016." mDiv="10" mFix="1" mStep="-1." massFrac="20.42" mfg="Contrail" peakThrust="1163.38" propWt="827." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>K-678-Sparky\r
+75mm/40 Inch Hardware\r
+2050cc\r
+Medium Nozzle\r
+</comments>\r
+<data>\r
+<eng-data cg="508." f="0." m="827." t="0."/>\r
+<eng-data cg="508." f="1163.38" m="825.546" t="0.00559284"/>\r
+<eng-data cg="508." f="444.822" m="31.4967" t="2.21477"/>\r
+<eng-data cg="508." f="256.628" m="14.8379" t="2.32103"/>\r
+<eng-data cg="508." f="102.651" m="9.44907" t="2.38814"/>\r
+<eng-data cg="508." f="0." m="0." t="2.8"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-K707 75 813 0 0.145 3.674 Contrail_Rockets \r
-0.0466102 281.209\r
-0.122881 1278.22\r
-0.165254 894.757\r
-0.495763 1431.61\r
-0.618644 1150.4\r
-0.694915 945.886\r
-0.834746 920.322\r
-1.01271 664.677\r
-1.50847 536.854\r
-1.62288 281.209\r
-1.72881 127.822\r
-2 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="1042.99" Itot="1391.04" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="695.518" burn-time="2." cgDiv="10" cgFix="1" cgStep="-1." code="K707" delays="1000" dia="75." exitDia="0." initWt="3674." len="1041.4" mDiv="10" mFix="1" mStep="-1." massFrac="3.7" mfg="Contrail" peakThrust="1351.58" propWt="136." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>K-707-BG Reload\r
+Medium Nozzle\r
+1400cc\r
+</comments>\r
+<data>\r
+<eng-data cg="520.7" f="0." m="136." t="0."/>\r
+<eng-data cg="520.7" f="684.342" m="135.626" t="0.0111857"/>\r
+<eng-data cg="520.7" f="1351.58" m="117.257" t="0.195749"/>\r
+<eng-data cg="520.7" f="1180.49" m="105.835" t="0.288031"/>\r
+<eng-data cg="520.7" f="1129.16" m="96.6783" t="0.369128"/>\r
+<eng-data cg="520.7" f="496.148" m="6.69454" t="1.50168"/>\r
+<eng-data cg="520.7" f="307.954" m="4.16624" t="1.566"/>\r
+<eng-data cg="520.7" f="171.085" m="2.52912" t="1.63591"/>\r
+<eng-data cg="520.7" f="119.76" m="1.85321" t="1.68345"/>\r
+<eng-data cg="520.7" f="0." m="0." t="2."/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-K777 75 1016 0 0.645 4.05 Contrail_Rockets \r
-0 931.023\r
-0.0950783 965.506\r
-0.111857 1793.08\r
-0.167785 1741.36\r
-0.206935 1344.81\r
-0.727069 1137.92\r
-1.00112 810.335\r
-1.97427 413.788\r
-2.04698 172.412\r
-2.6 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="292.44" Itot="1849.8" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="711.462" burn-time="2.6" cgDiv="10" cgFix="1" cgStep="-1." code="K777" delays="1000" dia="75." exitDia="0." initWt="4050." len="1016." mDiv="10" mFix="1" mStep="-1." massFrac="15.93" mfg="Contrail" peakThrust="1793.08" propWt="645." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="508." f="0." m="645." t="0."/>\r
+<eng-data cg="508." f="931.023" m="645." t="0."/>\r
+<eng-data cg="508." f="965.506" m="613.563" t="0.0950783"/>\r
+<eng-data cg="508." f="1793.08" m="605.493" t="0.111857"/>\r
+<eng-data cg="508." f="1741.36" m="571.03" t="0.167785"/>\r
+<eng-data cg="508." f="1344.81" m="549.965" t="0.206935"/>\r
+<eng-data cg="508." f="1137.92" m="324.827" t="0.727069"/>\r
+<eng-data cg="508." f="810.335" m="231.741" t="1.00112"/>\r
+<eng-data cg="508." f="413.788" m="24.0541" t="1.97427"/>\r
+<eng-data cg="508." f="172.412" m="16.6231" t="2.04698"/>\r
+<eng-data cg="508." f="0." m="0." t="2.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="119.38" Itot="2458.58" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="910.585" burn-time="2.7" cgDiv="10" cgFix="1" cgStep="-1." code="K888" delays="1000" dia="75." exitDia="0." initWt="4100." len="990.6" mDiv="10" mFix="1" mStep="-1." massFrac="51.22" mfg="Contrail" peakThrust="1365." propWt="2100." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Contrail Rockets Hybrid Rocket Motor (K888)\r
+75mm-2000cc Hardware with Medium Injector Kit and Nozzle\r
+Black Smoke Reload\r
+Data Input By Tom R. Sanders of Contrail Rockets LLC.\r
+</comments>\r
+<data>\r
+<eng-data cg="495.3" f="0." m="2100." t="0."/>\r
+<eng-data cg="495.3" f="1365." m="2100." t="0."/>\r
+<eng-data cg="495.3" f="1365." m="1517.04" t="0.5"/>\r
+<eng-data cg="495.3" f="1069.77" m="954.045" t="1.04143"/>\r
+<eng-data cg="495.3" f="434.109" m="19.0464" t="2.4972"/>\r
+<eng-data cg="495.3" f="124.031" m="8.3699" t="2.54199"/>\r
+<eng-data cg="495.3" f="0." m="0." t="2.7"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Contrail Rockets LLC Hybrid Rocket Motor (L1222)\r
-;75mm-3200cc Motor System\r
-;Sparky Hybrid Fuel\r
-;Data Input By Tom R. Sanders of Contrail Rockets\r
-L1222 75 1339.85 0 3.9 4.989 Contrail_Rockets \r
-0 455\r
-0.25 455\r
-0.5 2725\r
-0.75 1816\r
-2.75 680\r
-3.1 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="96.58" Itot="3693.88" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1191.57" burn-time="3.1" cgDiv="10" cgFix="1" cgStep="-1." code="L1222" delays="1000" dia="75." exitDia="0." initWt="4989." len="1339.85" mDiv="10" mFix="1" mStep="-1." massFrac="78.17" mfg="Contrail" peakThrust="2725." propWt="3900." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Contrail Rockets LLC Hybrid Rocket Motor (L1222)\r
+75mm-3200cc Motor System\r
+Sparky Hybrid Fuel\r
+Data Input By Tom R. Sanders of Contrail Rockets\r
+</comments>\r
+<data>\r
+<eng-data cg="669.925" f="0." m="3900." t="0."/>\r
+<eng-data cg="669.925" f="455." m="3900." t="0."/>\r
+<eng-data cg="669.925" f="455." m="3779.9" t="0.25"/>\r
+<eng-data cg="669.925" f="2725." m="3360.22" t="0.5"/>\r
+<eng-data cg="669.925" f="1816." m="2760.92" t="0.75"/>\r
+<eng-data cg="669.925" f="680." m="125.64" t="2.75"/>\r
+<eng-data cg="669.925" f="0." m="0." t="3.1"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="139.29" Itot="4781.05" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1542.28" burn-time="3.1" cgDiv="10" cgFix="1" cgStep="-1." code="L1428" delays="1000" dia="75." exitDia="0." initWt="5738." len="1492.25" mDiv="10" mFix="1" mStep="-1." massFrac="61." mfg="Contrail" peakThrust="2751.94" propWt="3500." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Contrail Rockets LLC. Hybrid Rocket Motor (L1428)\r
+75mm-3200cc Motor Using Fast Injector Kit and Nozzle\r
+Data Input By Tom R. Sanders of Contrail Rockets\r
+</comments>\r
+<data>\r
+<eng-data cg="746.125" f="0." m="3500." t="0."/>\r
+<eng-data cg="746.125" f="1425." m="3500." t="0."/>\r
+<eng-data cg="746.125" f="2751.94" m="2883.66" t="0.403135"/>\r
+<eng-data cg="746.125" f="2725." m="2088.06" t="0.8"/>\r
+<eng-data cg="746.125" f="1511.63" m="1453.17" t="1.20941"/>\r
+<eng-data cg="746.125" f="800." m="234.258" t="2.65"/>\r
+<eng-data cg="746.125" f="800." m="29.2823" t="3."/>\r
+<eng-data cg="746.125" f="0." m="0." t="3.1"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-L2525 75 1492.25 0 3.5 5.579 Contrail_Rockets \r
-0 4200\r
-0.754759 3294.57\r
-1.9 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="137.37" Itot="4714.84" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2481.49" burn-time="1.9" cgDiv="10" cgFix="1" cgStep="-1." code="L2525" delays="1000" dia="75." exitDia="0." initWt="5579." len="1492.25" mDiv="10" mFix="1" mStep="-1." massFrac="62.74" mfg="Contrail" peakThrust="4200." propWt="3500." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="746.125" f="0." m="3500." t="0."/>\r
+<eng-data cg="746.125" f="4200." m="3500." t="0."/>\r
+<eng-data cg="746.125" f="3294.57" m="1400.45" t="0.754759"/>\r
+<eng-data cg="746.125" f="0." m="0." t="1.9"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;L-369-Sparky\r
-;Slow nozzle\r
-;75mm/54 Inch Hardware\r
-;3200cc\r
-L369 75 1371.6 0 0.514 4.8 Contrail_Rockets \r
-0.0223714 540.63\r
-1.45414 533.787\r
-8.92617 260.05\r
-9.08277 130.025\r
-9.28412 68.4342\r
-10.6 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="761.12" Itot="3836.54" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="361.938" burn-time="10.6" cgDiv="10" cgFix="1" cgStep="-1." code="L369" delays="1000" dia="75." exitDia="0." initWt="4800." len="1371.6" mDiv="10" mFix="1" mStep="-1." massFrac="10.71" mfg="Contrail" peakThrust="540.63" propWt="514." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>L-369-Sparky\r
+Slow nozzle\r
+75mm/54 Inch Hardware\r
+3200cc\r
+</comments>\r
+<data>\r
+<eng-data cg="685.8" f="0." m="514." t="0."/>\r
+<eng-data cg="685.8" f="540.63" m="513.19" t="0.0223714"/>\r
+<eng-data cg="685.8" f="533.787" m="410.142" t="1.45414"/>\r
+<eng-data cg="685.8" f="260.05" m="12.8011" t="8.92617"/>\r
+<eng-data cg="685.8" f="130.025" m="8.7091" t="9.08277"/>\r
+<eng-data cg="685.8" f="68.4342" m="6.0323" t="9.28412"/>\r
+<eng-data cg="685.8" f="0." m="0." t="10.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;L-800-Sparky\r
-;75mm/54 Inch Hardware\r
-;3200cc\r
-;Medium Nozzle\r
-L800 75 1371.6 0 0.988 4.726 Contrail_Rockets \r
-0.00559284 1351.58\r
-0.167785 1129.16\r
-0.329978 1266.03\r
-0.553691 1248.92\r
-0.665548 1129.16\r
-3.48434 821.21\r
-3.5962 496.148\r
-3.69687 273.737\r
-3.83669 153.977\r
-4.6 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="388.43" Itot="3763.46" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="818.143" burn-time="4.6" cgDiv="10" cgFix="1" cgStep="-1." code="L800" delays="1000" dia="75." exitDia="0." initWt="4726." len="1371.6" mDiv="10" mFix="1" mStep="-1." massFrac="20.91" mfg="Contrail" peakThrust="1351.58" propWt="988." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>L-800-Sparky\r
+75mm/54 Inch Hardware\r
+3200cc\r
+Medium Nozzle\r
+</comments>\r
+<data>\r
+<eng-data cg="685.8" f="0." m="988." t="0."/>\r
+<eng-data cg="685.8" f="1351.58" m="987.008" t="0.00559284"/>\r
+<eng-data cg="685.8" f="1129.16" m="934.194" t="0.167785"/>\r
+<eng-data cg="685.8" f="1266.03" m="883.2" t="0.329978"/>\r
+<eng-data cg="685.8" f="1248.92" m="809.349" t="0.553691"/>\r
+<eng-data cg="685.8" f="1129.16" m="774.432" t="0.665548"/>\r
+<eng-data cg="685.8" f="821.21" m="52.7936" t="3.48434"/>\r
+<eng-data cg="685.8" f="496.148" m="33.4508" t="3.5962"/>\r
+<eng-data cg="685.8" f="273.737" m="23.2774" t="3.69687"/>\r
+<eng-data cg="685.8" f="153.977" m="15.4275" t="3.83669"/>\r
+<eng-data cg="685.8" f="0." m="0." t="4.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="148.69" Itot="5613.91" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1675.79" burn-time="3.35" cgDiv="10" cgFix="1" cgStep="-1." code="M1491" delays="1000" dia="75." exitDia="0." initWt="4876." len="1339.85" mDiv="10" mFix="1" mStep="-1." massFrac="78.96" mfg="Contrail" peakThrust="2725." propWt="3850." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Contrail Rockets LLC. Hybrid Rocket Motor (M1491\r
+75mm-3200cc Motor Using Medium Injector Kit and Nozzle\r
+Data Input By Tom R. Sanders of Contrail Rockets\r
+</comments>\r
+<data>\r
+<eng-data cg="669.925" f="0." m="3850." t="0."/>\r
+<eng-data cg="669.925" f="2725." m="3850." t="0."/>\r
+<eng-data cg="669.925" f="2635.66" m="2964.88" t="0.481523"/>\r
+<eng-data cg="669.925" f="2286.82" m="2407.29" t="0.81187"/>\r
+<eng-data cg="669.925" f="1860.47" m="1666.77" t="1.33259"/>\r
+<eng-data cg="669.925" f="900." m="88.4663" t="3."/>\r
+<eng-data cg="669.925" f="503.876" m="44.7997" t="3.09071"/>\r
+<eng-data cg="669.925" f="0." m="0." t="3.35"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;M-1575-Black Gold Reload\r
-;5300cc\r
-;98mm/60 Inch Hardware\r
-M1575 98 1524 0 0.726 10.863 Contrail_Rockets \r
-0.139821 2429.41\r
-0.503356 2976.89\r
-2.95302 1402.9\r
-3.06488 923.861\r
-3.21029 376.388\r
-3.31096 205.303\r
-4.2 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="963.85" Itot="6862.25" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1633.87" burn-time="4.2" cgDiv="10" cgFix="1" cgStep="-1." code="M1575" delays="1000" dia="98." exitDia="0." initWt="10863." len="1524." mDiv="10" mFix="1" mStep="-1." massFrac="6.68" mfg="Contrail" peakThrust="2976.89" propWt="726." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>M-1575-Black Gold Reload\r
+5300cc\r
+98mm/60 Inch Hardware\r
+</comments>\r
+<data>\r
+<eng-data cg="762." f="0." m="726." t="0."/>\r
+<eng-data cg="762." f="2429.41" m="708.031" t="0.139821"/>\r
+<eng-data cg="762." f="2976.89" m="604.067" t="0.503356"/>\r
+<eng-data cg="762." f="1402.9" m="36.522" t="2.95302"/>\r
+<eng-data cg="762." f="923.861" m="22.7542" t="3.06488"/>\r
+<eng-data cg="762." f="376.388" m="12.7528" t="3.21029"/>\r
+<eng-data cg="762." f="205.303" m="9.6551" t="3.31096"/>\r
+<eng-data cg="762." f="0." m="0." t="4.2"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="142.92" Itot="5536.15" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2586.99" burn-time="2.14" cgDiv="10" cgFix="1" cgStep="-1." code="M2281" delays="1000" dia="75." exitDia="0." initWt="5579." len="1492.25" mDiv="10" mFix="1" mStep="-1." massFrac="70.8" mfg="Contrail" peakThrust="4550." propWt="3950." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Contrail Rockets LLC. Hybrid Rocket Motor (M2281)\r
+75mm-3200cc Motor Using Fast Injector Kit and Nozzle\r
+Data Input By Tom R. Sanders of Contrail Rockets\r
+</comments>\r
+<data>\r
+<eng-data cg="746.125" f="0." m="3950." t="0."/>\r
+<eng-data cg="746.125" f="2725." m="3950." t="0."/>\r
+<eng-data cg="746.125" f="4550." m="3430.93" t="0.2"/>\r
+<eng-data cg="746.125" f="4550." m="2132.38" t="0.6"/>\r
+<eng-data cg="746.125" f="4550." m="1483.1" t="0.8"/>\r
+<eng-data cg="746.125" f="4000." m="1178.08" t="0.9"/>\r
+<eng-data cg="746.125" f="2725." m="1058.13" t="0.95"/>\r
+<eng-data cg="746.125" f="116.279" m="6.31855" t="1.98768"/>\r
+<eng-data cg="746.125" f="0." m="0." t="2.14"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-M2700 98 1524 0 0.412 10.432 Contrail_Rockets \r
-0.00847458 2965.48\r
-0.0508475 3272.26\r
-0.105932 5930.96\r
-0.347458 5828.7\r
-0.504237 6442.25\r
-0.512712 5726.45\r
-0.601695 5112.9\r
-0.745763 3681.29\r
-0.902542 3067.74\r
-1.06356 2454.19\r
-1.18644 1942.9\r
-1.34322 1738.39\r
-1.75 715.806\r
-1.95763 102.258\r
-2.3 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="0." Itot="6081.49" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2644.13" burn-time="2.3" cgDiv="10" cgFix="1" cgStep="-1." code="M2700" delays="1000" dia="98." exitDia="0." initWt="10432." len="1524." mDiv="10" mFix="1" mStep="-1." massFrac="0." mfg="Contrail" peakThrust="6442.25" propWt="412." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="0." f="0." m="0." t="0."/>\r
+<eng-data cg="0." f="2965.48" m="0." t="0.00847458"/>\r
+<eng-data cg="0." f="3272.26" m="0." t="0.0508475"/>\r
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+<eng-data cg="0." f="5828.7" m="0." t="0.347458"/>\r
+<eng-data cg="0." f="6442.25" m="0." t="0.504237"/>\r
+<eng-data cg="0." f="5726.45" m="0." t="0.512712"/>\r
+<eng-data cg="0." f="5112.9" m="0." t="0.601695"/>\r
+<eng-data cg="0." f="3681.29" m="0." t="0.745763"/>\r
+<eng-data cg="0." f="3067.74" m="0." t="0.902542"/>\r
+<eng-data cg="0." f="2454.19" m="0." t="1.06356"/>\r
+<eng-data cg="0." f="1942.9" m="0." t="1.18644"/>\r
+<eng-data cg="0." f="1738.39" m="0." t="1.34322"/>\r
+<eng-data cg="0." f="715.806" m="0." t="1.75"/>\r
+<eng-data cg="0." f="102.258" m="0." t="1.95763"/>\r
+<eng-data cg="0." f="0." m="0." t="2.3"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;M-2800-Black Gold Reload\r
-;5300cc\r
-;98mm/60 inch Hardware\r
-M2800 98 1524 0 0.476 10.704 Contrail_Rockets \r
-0.00838926 2395.2\r
-0.251678 2805.8\r
-0.545302 3695.45\r
-0.75783 5611.6\r
-0.911633 4311.35\r
-1.1745 3558.58\r
-1.4094 2258.33\r
-1.70861 1505.55\r
-2.3 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="1301.45" Itot="6075.12" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2641.36" burn-time="2.3" cgDiv="10" cgFix="1" cgStep="-1." code="M2800" delays="1000" dia="98." exitDia="0." initWt="10704." len="1524." mDiv="10" mFix="1" mStep="-1." massFrac="4.45" mfg="Contrail" peakThrust="5611.6" propWt="476." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>M-2800-Black Gold Reload\r
+5300cc\r
+98mm/60 inch Hardware\r
+</comments>\r
+<data>\r
+<eng-data cg="762." f="0." m="476." t="0."/>\r
+<eng-data cg="762." f="2395.2" m="475.213" t="0.00838926"/>\r
+<eng-data cg="762." f="2805.8" m="425.641" t="0.251678"/>\r
+<eng-data cg="762." f="3695.45" m="350.857" t="0.545302"/>\r
+<eng-data cg="762." f="5611.6" m="273.366" t="0.75783"/>\r
+<eng-data cg="762." f="4311.35" m="213.576" t="0.911633"/>\r
+<eng-data cg="762." f="3558.58" m="132.531" t="1.1745"/>\r
+<eng-data cg="762." f="2258.33" m="79.001" t="1.4094"/>\r
+<eng-data cg="762." f="1505.55" m="34.8812" t="1.70861"/>\r
+<eng-data cg="762." f="0." m="0." t="2.3"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="135.22" Itot="5569.64" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="771.418" burn-time="7.22" cgDiv="10" cgFix="1" cgStep="-1." code="M711" delays="1000" dia="75." exitDia="0." initWt="4900." len="1340." mDiv="10" mFix="1" mStep="-1." massFrac="85.71" mfg="Contrail" peakThrust="1140." propWt="4200." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Contrail Rockets LLC Hybrid Rocket Motor. (M-711)\r
+75-3200cc Hardware Set\r
+Black Smoke Fuel\r
+</comments>\r
+<data>\r
+<eng-data cg="670." f="0." m="4200." t="0."/>\r
+<eng-data cg="670." f="1140." m="4200." t="0."/>\r
+<eng-data cg="670." f="1069.77" m="2977.75" t="1.46697"/>\r
+<eng-data cg="670." f="680." m="1306.6" t="4."/>\r
+<eng-data cg="670." f="589.147" m="123.423" t="6.47256"/>\r
+<eng-data cg="670." f="279.07" m="57.4374" t="6.67413"/>\r
+<eng-data cg="670." f="0." m="0." t="7.22"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-O6300 152 1828.8 0 3.175 28.576 Contrail_Rockets \r
-0.0338983 12271\r
-0.728814 9714.51\r
-1.65254 9203.22\r
-2.37288 8947.57\r
-2.51695 6646.77\r
-2.78814 4601.61\r
-2.99153 4857.25\r
-3.27966 3579.03\r
-3.61017 1278.22\r
-4.29 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="937.33" Itot="29184.8" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="6802.98" burn-time="4.29" cgDiv="10" cgFix="1" cgStep="-1." code="O6300" delays="1000" dia="152." exitDia="0." initWt="28576." len="1828.8" mDiv="10" mFix="1" mStep="-1." massFrac="11.11" mfg="Contrail Rockets" peakThrust="12271." propWt="3175." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="914.4" f="0." m="3175." t="0."/>\r
+<eng-data cg="914.4" f="12271." m="3152.37" t="0.0338983"/>\r
+<eng-data cg="914.4" f="9714.51" m="2321.33" t="0.728814"/>\r
+<eng-data cg="914.4" f="9203.22" m="1370.79" t="1.65254"/>\r
+<eng-data cg="914.4" f="8947.57" m="659.592" t="2.37288"/>\r
+<eng-data cg="914.4" f="6646.77" m="537.386" t="2.51695"/>\r
+<eng-data cg="914.4" f="4601.61" m="371.46" t="2.78814"/>\r
+<eng-data cg="914.4" f="4857.25" m="266.814" t="2.99153"/>\r
+<eng-data cg="914.4" f="3579.03" m="134.591" t="3.27966"/>\r
+<eng-data cg="914.4" f="1278.22" m="47.2678" t="3.61017"/>\r
+<eng-data cg="914.4" f="0." m="0." t="4.29"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+E12EM 24 101 0-4-8 0.02800 0.05320 EM\r
+ 0.01 31.17 \r
+ 0.13 24.43 \r
+ 0.17 23.34 \r
+ 1.50 14.83 \r
+ 2.00 10.28 \r
+ 2.50 4.80 \r
+ 2.91 2.30 \r
+ 2.92 0.00 \r
+;\r
--- /dev/null
+F23EM 24 139 0-4-8 0.04760 0.07560 EM\r
+ 0.01 24.19 \r
+ 0.05 39.00 \r
+ 0.07 39.14 \r
+ 0.13 34.58 \r
+ 1.00 26.94 \r
+ 2.00 19.52 \r
+ 2.40 14.00 \r
+ 2.70 7.96 \r
+ 3.00 4.46 \r
+ 3.55 1.27 \r
+ 3.58 0.00 \r
+;\r
+++ /dev/null
-;\r
-G20 29 149 3 0.0729 0.1179 Ellis_Mountain \r
-0.0463679 46.6843\r
-0.278207 30.3888\r
-0.479134 26.8655\r
-1.00464 24.6634\r
-3.47759 22.0209\r
-4.32767 13.653\r
-5.11592 3.08293\r
-5.47 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="152.94" Itot="109.337" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="19.988" burn-time="5.47" cgDiv="10" cgFix="1" cgStep="-1." code="G20" delays="3" dia="29." exitDia="0." initWt="117.9" len="149." mDiv="10" mFix="1" mStep="-1." massFrac="61.83" mfg="Ellis Mountain" peakThrust="46.684" propWt="72.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <data>\r
+ <eng-data cg="74.5" f="0." m="72.9" t="0."/>\r
+ <eng-data cg="74.5" f="46.6843" m="72.1784" t="0.0463679"/>\r
+ <eng-data cg="74.5" f="30.3888" m="66.2214" t="0.278207"/>\r
+ <eng-data cg="74.5" f="26.8655" m="62.3863" t="0.479134"/>\r
+ <eng-data cg="74.5" f="24.6634" m="53.359" t="1.00464"/>\r
+ <eng-data cg="74.5" f="22.0209" m="14.8716" t="3.47759"/>\r
+ <eng-data cg="74.5" f="13.653" m="4.76182" t="4.32767"/>\r
+ <eng-data cg="74.5" f="3.08293" m="0.363913" t="5.11592"/>\r
+ <eng-data cg="74.5" f="0." m="-0." t="5.47"/>\r
+ </data>\r
+ </engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Ellis Mountain G35 Single Use Motor\r
-G35EM 29 165 6-10 0.082 0.135 Ellis_Mountain \r
-0.01 51.12\r
-0.04 57.55\r
-0.08 43.78\r
-2.73 28.16\r
-3.28 28.16\r
-3.78 6.73\r
-4 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="154.43" Itot="124.184" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="31.046" burn-time="4." cgDiv="10" cgFix="1" cgStep="-1." code="G35EM" delays="6,10" dia="29." exitDia="0." initWt="135." len="165." mDiv="10" mFix="1" mStep="-1." massFrac="60.74" mfg="Ellis Mountain" peakThrust="57.55" propWt="82." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <comments>Ellis Mountain G35 Single Use Motor</comments>\r
+ <data>\r
+ <eng-data cg="82.5" f="0." m="82." t="0."/>\r
+ <eng-data cg="82.5" f="51.12" m="81.8312" t="0.01"/>\r
+ <eng-data cg="82.5" f="57.55" m="80.7549" t="0.04"/>\r
+ <eng-data cg="82.5" f="43.78" m="79.4167" t="0.08"/>\r
+ <eng-data cg="82.5" f="28.16" m="16.4753" t="2.73"/>\r
+ <eng-data cg="82.5" f="28.16" m="6.24841" t="3.28"/>\r
+ <eng-data cg="82.5" f="6.73" m="0.48883" t="3.78"/>\r
+ <eng-data cg="82.5" f="0." m="-0." t="4."/>\r
+ </data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-G37 24 181 6-10-100 0.068 0.1133 Ellis_Mountain \r
-0.0231839 69.586\r
-0.162287 55.9331\r
-0.332303 48.0056\r
-0.502318 44.9226\r
-0.996909 40.9589\r
-1.49923 38.7568\r
-2.00155 34.3526\r
-2.49614 28.1868\r
-2.75116 18.4976\r
-2.99845 5.28502\r
-3.1 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="165.74" Itot="110.521" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="35.652" burn-time="3.1" cgDiv="10" cgFix="1" cgStep="-1." code="G37" delays="6,10,1000" dia="24." exitDia="0." initWt="113.3" len="181." mDiv="10" mFix="1" mStep="-1." massFrac="60.02" mfg="Ellis Mountain" peakThrust="69.586" propWt="68." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+ <eng-data cg="90.5" f="0." m="68." t="0."/>\r
+ <eng-data cg="90.5" f="69.586" m="67.5037" t="0.0231839"/>\r
+ <eng-data cg="90.5" f="55.9331" m="62.1324" t="0.162287"/>\r
+ <eng-data cg="90.5" f="48.0056" m="56.6961" t="0.332303"/>\r
+ <eng-data cg="90.5" f="44.9226" m="51.8357" t="0.502318"/>\r
+ <eng-data cg="90.5" f="40.9589" m="38.7686" t="0.996909"/>\r
+ <eng-data cg="90.5" f="38.7568" m="26.4501" t="1.49923"/>\r
+ <eng-data cg="90.5" f="34.3526" m="15.1524" t="2.00155"/>\r
+ <eng-data cg="90.5" f="28.1868" m="5.63689" t="2.49614"/>\r
+ <eng-data cg="90.5" f="18.4976" m="1.97436" t="2.75116"/>\r
+ <eng-data cg="90.5" f="5.28502" m="0.165105" t="2.99845"/>\r
+ <eng-data cg="90.5" f="0." m="-0." t="3.1"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-H275 29 275 10 0.142 0.255 Ellis_Mountain \r
-0.0123648 792.752\r
-0.015456 356.739\r
-0.197836 312.697\r
-0.797527 268.655\r
-0.911901 255.442\r
-0.992272 123.317\r
-1.04173 39.6376\r
-1.1 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="209.99" Itot="292.416" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="265.833" burn-time="1.1" cgDiv="10" cgFix="1" cgStep="-1." code="H275" delays="10" dia="29." exitDia="0." initWt="255." len="275." mDiv="10" mFix="1" mStep="-1." massFrac="55.69" mfg="Ellis Mountain" peakThrust="792.752" propWt="142." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="137.5" f="0." m="142." t="0."/>\r
+<eng-data cg="137.5" f="792.752" m="139.62" t="0.0123648"/>\r
+<eng-data cg="137.5" f="356.739" m="138.757" t="0.015456"/>\r
+<eng-data cg="137.5" f="312.697" m="109.113" t="0.197836"/>\r
+<eng-data cg="137.5" f="268.655" m="24.4634" t="0.797527"/>\r
+<eng-data cg="137.5" f="255.442" m="9.90894" t="0.911901"/>\r
+<eng-data cg="137.5" f="123.317" m="2.51766" t="0.992272"/>\r
+<eng-data cg="137.5" f="39.6376" m="0.560802" t="1.04173"/>\r
+<eng-data cg="137.5" f="0." m="-0." t="1.1"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Ellis Mountain Rocket Works\r
-;H48 Single Use motor\r
-H48 38 200 8-100 0.154 0.292 Ellis_Mountain \r
-0.05 101.5\r
-0.1 101.5\r
-0.21 92.18\r
-0.46 86.48\r
-0.74 83.38\r
-1 80\r
-1.49 74.57\r
-1.99 68.36\r
-2.48 63.18\r
-2.99 56.45\r
-3.2 34.18\r
-3.5 18\r
-3.69 13.46\r
-4 11\r
-4.36 7.77\r
-4.4 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="165.28" Itot="249.609" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="56.729" burn-time="4.4" cgDiv="10" cgFix="1" cgStep="-1." code="H48" delays="1000" dia="38." exitDia="0." initWt="292." len="200." mDiv="10" mFix="1" mStep="-1." massFrac="52.74" mfg="Ellis Mountain" peakThrust="101.5" propWt="154." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Ellis Mountain Rocket Works\r
+H48 Single Use motor\r
+</comments>\r
+<data>\r
+<eng-data cg="100." f="0." m="154." t="0."/>\r
+<eng-data cg="100." f="101.5" m="152.434" t="0.05"/>\r
+<eng-data cg="100." f="101.5" m="149.303" t="0.1"/>\r
+<eng-data cg="100." f="92.18" m="142.731" t="0.21"/>\r
+<eng-data cg="100." f="86.48" m="128.953" t="0.46"/>\r
+<eng-data cg="100." f="83.38" m="114.281" t="0.74"/>\r
+<eng-data cg="100." f="80." m="101.177" t="1."/>\r
+<eng-data cg="100." f="74.57" m="77.8131" t="1.49"/>\r
+<eng-data cg="100." f="68.36" m="55.7674" t="1.99"/>\r
+<eng-data cg="100." f="63.18" m="35.8843" t="2.48"/>\r
+<eng-data cg="100." f="56.45" m="17.0635" t="2.99"/>\r
+<eng-data cg="100." f="34.18" m="11.1923" t="3.2"/>\r
+<eng-data cg="100." f="18." m="6.36336" t="3.5"/>\r
+<eng-data cg="100." f="13.46" m="4.51945" t="3.69"/>\r
+<eng-data cg="100." f="11." m="2.18035" t="4."/>\r
+<eng-data cg="100." f="7.77" m="0.0958762" t="4.36"/>\r
+<eng-data cg="100." f="0." m="-0." t="4.4"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Ellis Mountain Rocket Works\r
-;H50 Single Use motor\r
-H50 29 279 6-10 0.163 0.3 Ellis_Mountain \r
-0.01 63.67\r
-0.17 108.9\r
-0.27 94.9\r
-0.47 81.43\r
-0.79 71.02\r
-1.27 64.9\r
-1.97 60.61\r
-2.56 56.94\r
-3.01 52.04\r
-3.52 45.31\r
-3.97 34.9\r
-4.49 18.37\r
-4.97 4.9\r
-5.28 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="165.88" Itot="265.152" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="50.218" burn-time="5.28" cgDiv="10" cgFix="1" cgStep="-1." code="H50" delays="6,10" dia="29." exitDia="0." initWt="300." len="279." mDiv="10" mFix="1" mStep="-1." massFrac="54.33" mfg="Ellis Mountain" peakThrust="108.9" propWt="163." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Ellis Mountain Rocket Works\r
+H50 Single Use motor\r
+</comments>\r
+<data>\r
+<eng-data cg="139.5" f="0." m="163." t="0."/>\r
+<eng-data cg="139.5" f="63.67" m="162.804" t="0.01"/>\r
+<eng-data cg="139.5" f="108.9" m="154.317" t="0.17"/>\r
+<eng-data cg="139.5" f="94.9" m="148.053" t="0.27"/>\r
+<eng-data cg="139.5" f="81.43" m="137.213" t="0.47"/>\r
+<eng-data cg="139.5" f="71.02" m="122.219" t="0.79"/>\r
+<eng-data cg="139.5" f="64.9" m="102.165" t="1.27"/>\r
+<eng-data cg="139.5" f="60.61" m="75.1606" t="1.97"/>\r
+<eng-data cg="139.5" f="56.94" m="53.8431" t="2.56"/>\r
+<eng-data cg="139.5" f="52.04" m="38.7693" t="3.01"/>\r
+<eng-data cg="139.5" f="45.31" m="23.5088" t="3.52"/>\r
+<eng-data cg="139.5" f="34.9" m="12.4144" t="3.97"/>\r
+<eng-data cg="139.5" f="18.37" m="3.90011" t="4.49"/>\r
+<eng-data cg="139.5" f="4.9" m="0.466896" t="4.97"/>\r
+<eng-data cg="139.5" f="0." m="-0." t="5.28"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-I130 38 330 100 0.308 0.625 Ellis_Mountain \r
-0.015456 266.453\r
-0.0540958 160.753\r
-0.502318 169.561\r
-2.23338 180.571\r
-2.48841 149.742\r
-2.99073 136.53\r
-3.49304 77.0732\r
-4.01082 26.4251\r
-4.43 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="194.47" Itot="587.39" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="132.594" burn-time="4.43" cgDiv="10" cgFix="1" cgStep="-1." code="I130" delays="1000" dia="38." exitDia="0." initWt="625." len="330." mDiv="10" mFix="1" mStep="-1." massFrac="49.28" mfg="Ellis Mountain" peakThrust="266.453" propWt="308." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="165." f="0." m="308." t="0."/>\r
+<eng-data cg="165." f="266.453" m="306.92" t="0.015456"/>\r
+<eng-data cg="165." f="160.753" m="302.592" t="0.0540958"/>\r
+<eng-data cg="165." f="169.561" m="263.776" t="0.502318"/>\r
+<eng-data cg="165." f="180.571" m="104.871" t="2.23338"/>\r
+<eng-data cg="165." f="149.742" m="82.7852" t="2.48841"/>\r
+<eng-data cg="165." f="136.53" m="45.0842" t="2.99073"/>\r
+<eng-data cg="165." f="77.0732" m="16.954" t="3.49304"/>\r
+<eng-data cg="165." f="26.4251" m="2.9041" t="4.01082"/>\r
+<eng-data cg="165." f="0." m="-0." t="4.43"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Ellis Mountain Rocket Works\r
-;I134 38mm Single Use motor\r
-I134 38 355 15 0.2807 0.5812 Ellis_Mountain \r
-0.1 268.8\r
-0.2 138\r
-1 116\r
-2 102\r
-3 85\r
-4 67\r
-4.65 16.46\r
-4.82 6.86\r
-5.07 6.86\r
-5.15 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="161.65" Itot="444.976" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="86.403" burn-time="5.15" cgDiv="10" cgFix="1" cgStep="-1." code="I134" delays="15" dia="38." exitDia="0." initWt="581.2" len="355." mDiv="10" mFix="1" mStep="-1." massFrac="48.3" mfg="Ellis Mountain" peakThrust="268.8" propWt="280.7" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Ellis Mountain Rocket Works\r
+I134 38mm Single Use motor\r
+</comments>\r
+<data>\r
+<eng-data cg="177.5" f="0." m="280.7" t="0."/>\r
+<eng-data cg="177.5" f="268.8" m="272.222" t="0.1"/>\r
+<eng-data cg="177.5" f="138." m="259.391" t="0.2"/>\r
+<eng-data cg="177.5" f="116." m="195.3" t="1."/>\r
+<eng-data cg="177.5" f="102." m="126.54" t="2."/>\r
+<eng-data cg="177.5" f="85." m="67.5584" t="3."/>\r
+<eng-data cg="177.5" f="67." m="19.6161" t="4."/>\r
+<eng-data cg="177.5" f="16.46" m="2.50537" t="4.65"/>\r
+<eng-data cg="177.5" f="6.86" m="1.25495" t="4.82"/>\r
+<eng-data cg="177.5" f="6.86" m="0.173097" t="5.07"/>\r
+<eng-data cg="177.5" f="0." m="-0." t="5.15"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Ellis Mountain I150\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I150 38 229 0 0.172032 0.425152 EM\r
- 0.050 101.298\r
- 0.152 159.193\r
- 0.255 169.686\r
- 0.358 179.603\r
- 0.460 188.152\r
- 0.564 193.364\r
- 0.667 204.520\r
- 0.769 212.046\r
- 0.872 212.937\r
- 0.975 208.076\r
- 1.077 196.555\r
- 1.180 191.025\r
- 1.283 186.106\r
- 1.386 181.835\r
- 1.490 177.947\r
- 1.592 175.877\r
- 1.695 173.744\r
- 1.798 170.664\r
- 1.900 161.823\r
- 2.003 149.111\r
- 2.106 124.923\r
- 2.208 68.392\r
- 2.311 20.122\r
- 2.415 7.794\r
- 2.518 4.464\r
- 2.621 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="226.13" Itot="380.979" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="142.689" burn-time="2.67" cgDiv="10" cgFix="1" cgStep="-1." code="I150" delays="20,1000" dia="38." exitDia="0." initWt="398.3" len="229." mDiv="10" mFix="1" mStep="-1." massFrac="43.13" mfg="Ellis Mountain" peakThrust="198.09" propWt="171.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="114.5" f="0." m="171.8" t="0."/>\r
+<eng-data cg="114.5" f="101.15" m="171.8" t="0."/>\r
+<eng-data cg="114.5" f="155.94" m="166.003" t="0.1"/>\r
+<eng-data cg="114.5" f="155.94" m="162.487" t="0.15"/>\r
+<eng-data cg="114.5" f="177.01" m="151.227" t="0.3"/>\r
+<eng-data cg="114.5" f="181.23" m="143.149" t="0.4"/>\r
+<eng-data cg="114.5" f="198.09" m="117.492" t="0.7"/>\r
+<eng-data cg="114.5" f="198.09" m="99.6262" t="0.9"/>\r
+<eng-data cg="114.5" f="181.23" m="82.521" t="1.1"/>\r
+<eng-data cg="114.5" f="160.15" m="20.9439" t="1.9"/>\r
+<eng-data cg="114.5" f="147.51" m="14.007" t="2."/>\r
+<eng-data cg="114.5" f="126.44" m="7.8302" t="2.1"/>\r
+<eng-data cg="114.5" f="21.07" m="1.17834" t="2.3"/>\r
+<eng-data cg="114.5" f="8.43" m="0.513196" t="2.4"/>\r
+<eng-data cg="114.5" f="0." m="-0." t="2.67"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Ellis Mountain I160\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I160 38 280 0 0.235648 0.528192 EM\r
- 0.068 169.405\r
- 0.206 199.425\r
- 0.346 205.072\r
- 0.485 206.075\r
- 0.624 205.840\r
- 0.763 204.052\r
- 0.902 200.850\r
- 1.042 200.885\r
- 1.180 203.053\r
- 1.319 204.157\r
- 1.458 206.392\r
- 1.598 210.051\r
- 1.736 212.769\r
- 1.875 211.177\r
- 2.015 207.500\r
- 2.154 189.766\r
- 2.293 136.149\r
- 2.431 52.306\r
- 2.571 42.841\r
- 2.710 41.803\r
- 2.849 33.042\r
- 2.987 24.614\r
- 3.127 17.154\r
- 3.267 7.477\r
- 3.406 1.777\r
- 3.546 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="216.61" Itot="492.608" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="151.572" burn-time="3.25" cgDiv="10" cgFix="1" cgStep="-1." code="I160" delays="1000" dia="38." exitDia="0." initWt="486.7" len="280." mDiv="10" mFix="1" mStep="-1." massFrac="47.65" mfg="Ellis Mountain" peakThrust="205.72" propWt="231.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="140." f="0." m="231.9" t="0."/>\r
+<eng-data cg="140." f="205.72" m="231.416" t="0.01"/>\r
+<eng-data cg="140." f="192.73" m="231.416" t="0.01"/>\r
+<eng-data cg="140." f="192.73" m="214.177" t="0.2"/>\r
+<eng-data cg="140." f="201.39" m="195.624" t="0.4"/>\r
+<eng-data cg="140." f="199.22" m="186.194" t="0.5"/>\r
+<eng-data cg="140." f="199.22" m="162.748" t="0.75"/>\r
+<eng-data cg="140." f="197.06" m="161.815" t="0.76"/>\r
+<eng-data cg="140." f="194.89" m="144.286" t="0.95"/>\r
+<eng-data cg="140." f="203.55" m="92.7046" t="1.5"/>\r
+<eng-data cg="140." f="199.22" m="26.3418" t="2.2"/>\r
+<eng-data cg="140." f="155.91" m="13.8033" t="2.35"/>\r
+<eng-data cg="140." f="41.14" m="11.4842" t="2.4"/>\r
+<eng-data cg="140." f="42.88" m="5.5512" t="2.7"/>\r
+<eng-data cg="140." f="0." m="-0." t="3.25"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Ellis Mountain I230\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I230 38 331 0 0.282688 0.620928 EM\r
- 0.058 292.627\r
- 0.178 317.660\r
- 0.298 309.874\r
- 0.418 305.243\r
- 0.537 299.679\r
- 0.657 298.170\r
- 0.777 294.591\r
- 0.897 293.800\r
- 1.018 289.736\r
- 1.138 288.222\r
- 1.257 284.614\r
- 1.377 281.149\r
- 1.497 274.879\r
- 1.617 269.775\r
- 1.736 258.925\r
- 1.856 242.249\r
- 1.976 207.607\r
- 2.097 136.698\r
- 2.217 86.506\r
- 2.336 74.324\r
- 2.456 51.246\r
- 2.576 45.546\r
- 2.696 27.050\r
- 2.816 6.382\r
- 2.936 1.423\r
- 3.057 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="218.61" Itot="625.988" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="221.197" burn-time="2.83" cgDiv="10" cgFix="1" cgStep="-1." code="I230" delays="20,1000" dia="38." exitDia="0." initWt="575.1" len="331." mDiv="10" mFix="1" mStep="-1." massFrac="50.77" mfg="Ellis Mountain" peakThrust="346.71" propWt="292." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="165.5" f="0." m="292." t="0."/>\r
+<eng-data cg="165.5" f="309.64" m="292." t="0."/>\r
+<eng-data cg="165.5" f="305.28" m="292." t="0."/>\r
+<eng-data cg="165.5" f="346.71" m="276.794" t="0.1"/>\r
+<eng-data cg="165.5" f="322.72" m="268.987" t="0.15"/>\r
+<eng-data cg="165.5" f="290.01" m="218.969" t="0.5"/>\r
+<eng-data cg="165.5" f="283.47" m="152.092" t="1."/>\r
+<eng-data cg="165.5" f="270.39" m="87.5037" t="1.5"/>\r
+<eng-data cg="165.5" f="252.94" m="63.0923" t="1.7"/>\r
+<eng-data cg="165.5" f="218.05" m="30.1374" t="2."/>\r
+<eng-data cg="165.5" f="82.86" m="12.592" t="2.25"/>\r
+<eng-data cg="165.5" f="78.5" m="6.94687" t="2.4"/>\r
+<eng-data cg="165.5" f="47.97" m="5.47203" t="2.45"/>\r
+<eng-data cg="165.5" f="43.61" m="2.26813" t="2.6"/>\r
+<eng-data cg="165.5" f="4.36" m="0.0305067" t="2.8"/>\r
+<eng-data cg="165.5" f="0." m="-0." t="2.83"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Ellis Mountain Rocket Works\r
-;I69 38mm Single Use motor\r
-I69 29 406 10 0.236 0.4 Ellis_Mountain \r
-0.05 78.67\r
-0.1 149.7\r
-0.25 133.5\r
-0.49 111.51\r
-0.75 100\r
-1.07 93.18\r
-1.48 87.83\r
-2 82.49\r
-2.5 78\r
-2.99 73.32\r
-3.5 64.5\r
-3.99 48.88\r
-4.5 29.79\r
-4.99 9.17\r
-5.28 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="159.51" Itot="369.166" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="69.918" burn-time="5.28" cgDiv="10" cgFix="1" cgStep="-1." code="I69" delays="10" dia="29." exitDia="0." initWt="400." len="406." mDiv="10" mFix="1" mStep="-1." massFrac="59." mfg="Ellis Mountain" peakThrust="149.7" propWt="236." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Ellis Mountain Rocket Works\r
+I69 38mm Single Use motor\r
+</comments>\r
+<data>\r
+<eng-data cg="203." f="0." m="236." t="0."/>\r
+<eng-data cg="203." f="78.67" m="234.743" t="0.05"/>\r
+<eng-data cg="203." f="149.7" m="231.093" t="0.1"/>\r
+<eng-data cg="203." f="133.5" m="217.515" t="0.25"/>\r
+<eng-data cg="203." f="111.51" m="198.719" t="0.49"/>\r
+<eng-data cg="203." f="100." m="181.141" t="0.75"/>\r
+<eng-data cg="203." f="93.18" m="161.382" t="1.07"/>\r
+<eng-data cg="203." f="87.83" m="137.66" t="1.48"/>\r
+<eng-data cg="203." f="82.49" m="109.351" t="2."/>\r
+<eng-data cg="203." f="78." m="83.7015" t="2.5"/>\r
+<eng-data cg="203." f="73.32" m="60.0013" t="2.99"/>\r
+<eng-data cg="203." f="64.5" m="37.5345" t="3.5"/>\r
+<eng-data cg="203." f="48.88" m="19.7765" t="3.99"/>\r
+<eng-data cg="203." f="29.79" m="6.95205" t="4.5"/>\r
+<eng-data cg="203." f="9.17" m="0.850016" t="4.99"/>\r
+<eng-data cg="203." f="0." m="-0." t="5.28"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J110 54 276.2 100 0.45359 0.8754 Ellis_Mountain \r
-0.108192 193.784\r
-0.386399 147.54\r
-1.00464 139.833\r
-4.034 116.711\r
-5.00773 94.6899\r
-6.01236 67.1637\r
-6.53787 37.4355\r
-6.8 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="169.06" Itot="751.993" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="110.587" burn-time="6.8" cgDiv="10" cgFix="1" cgStep="-1." code="J110" delays="1000" dia="54." exitDia="0." initWt="875.4" len="276.2" mDiv="10" mFix="1" mStep="-1." massFrac="51.82" mfg="Ellis Mountain" peakThrust="193.784" propWt="453.59" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="138.1" f="0." m="453.59" t="0."/>\r
+<eng-data cg="138.1" f="193.784" m="447.267" t="0.108192"/>\r
+<eng-data cg="138.1" f="147.54" m="418.628" t="0.386399"/>\r
+<eng-data cg="138.1" f="139.833" m="365.046" t="1.00464"/>\r
+<eng-data cg="138.1" f="116.711" m="130.659" t="4.034"/>\r
+<eng-data cg="138.1" f="94.6899" m="68.5771" t="5.00773"/>\r
+<eng-data cg="138.1" f="67.1637" m="19.5374" t="6.01236"/>\r
+<eng-data cg="138.1" f="37.4355" m="2.95951" t="6.53787"/>\r
+<eng-data cg="138.1" f="0." m="-0." t="6.8"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J148 54 355.6 14 0.67 1.179 Ellis_Mountain \r
-0.139104 218.007\r
-0.231839 183.875\r
-0.448223 171.763\r
-1.00464 170.662\r
-2.10201 170.662\r
-5.02318 147.54\r
-5.31685 133.226\r
-5.67233 49.547\r
-6.1 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="137.57" Itot="903.887" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="148.178" burn-time="6.1" cgDiv="10" cgFix="1" cgStep="-1." code="J148" delays="14" dia="54." exitDia="0." initWt="1179." len="355.6" mDiv="10" mFix="1" mStep="-1." massFrac="56.83" mfg="Ellis Mountain" peakThrust="218.007" propWt="670." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="177.8" f="0." m="670." t="0."/>\r
+<eng-data cg="177.8" f="218.007" m="658.761" t="0.139104"/>\r
+<eng-data cg="177.8" f="183.875" m="644.948" t="0.231839"/>\r
+<eng-data cg="177.8" f="171.763" m="616.427" t="0.448223"/>\r
+<eng-data cg="177.8" f="170.662" m="545.812" t="1.00464"/>\r
+<eng-data cg="177.8" f="170.662" m="406.993" t="2.10201"/>\r
+<eng-data cg="177.8" f="147.54" m="62.4921" t="5.02318"/>\r
+<eng-data cg="177.8" f="133.226" m="31.9334" t="5.31685"/>\r
+<eng-data cg="177.8" f="49.547" m="7.85338" t="5.67233"/>\r
+<eng-data cg="177.8" f="0." m="-0." t="6.1"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J228 38 562 6 0.27 0.8391 Ellis_Mountain \r
-0.0309119 665.031\r
-0.0927357 444.822\r
-0.262751 356.739\r
-0.664606 343.526\r
-0.989181 317.101\r
-1.96291 259.847\r
-2.99845 193.784\r
-4.01855 118.913\r
-4.99227 35.2334\r
-5.2 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="420.96" Itot="1114.61" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="214.348" burn-time="5.2" cgDiv="10" cgFix="1" cgStep="-1." code="J228" delays="6" dia="38." exitDia="0." initWt="839.1" len="562." mDiv="10" mFix="1" mStep="-1." massFrac="32.18" mfg="Ellis Mountain" peakThrust="665.031" propWt="270." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="281." f="0." m="270." t="0."/>\r
+<eng-data cg="281." f="665.031" m="267.51" t="0.0309119"/>\r
+<eng-data cg="281." f="444.822" m="259.2" t="0.0927357"/>\r
+<eng-data cg="281." f="356.739" m="242.694" t="0.262751"/>\r
+<eng-data cg="281." f="343.526" m="208.61" t="0.664606"/>\r
+<eng-data cg="281." f="317.101" m="182.64" t="0.989181"/>\r
+<eng-data cg="281." f="259.847" m="114.596" t="1.96291"/>\r
+<eng-data cg="281." f="193.784" m="57.7005" t="2.99845"/>\r
+<eng-data cg="281." f="118.913" m="19.0658" t="4.01855"/>\r
+<eng-data cg="281." f="35.2334" m="0.886472" t="4.99227"/>\r
+<eng-data cg="281." f="0." m="-0." t="5.2"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Ellis Mountain J270\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J270 38 384 0 0.341824 0.711872 EM\r
- 0.057 357.607\r
- 0.175 386.516\r
- 0.294 368.069\r
- 0.412 360.627\r
- 0.530 356.068\r
- 0.648 353.900\r
- 0.767 351.910\r
- 0.885 349.900\r
- 1.003 348.675\r
- 1.121 347.552\r
- 1.240 343.075\r
- 1.358 338.000\r
- 1.476 330.566\r
- 1.594 315.474\r
- 1.712 293.325\r
- 1.831 266.102\r
- 1.949 184.040\r
- 2.067 131.638\r
- 2.185 109.171\r
- 2.304 89.570\r
- 2.422 74.945\r
- 2.540 55.700\r
- 2.658 31.860\r
- 2.777 17.751\r
- 2.896 10.109\r
- 3.015 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="215.41" Itot="733.227" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="252.837" burn-time="2.9" cgDiv="10" cgFix="1" cgStep="-1." code="J270" delays="20,1000" dia="38." exitDia="0." initWt="686.8" len="384." mDiv="10" mFix="1" mStep="-1." massFrac="50.54" mfg="Ellis Mountain" peakThrust="441.3" propWt="347.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="192." f="0." m="347.1" t="0."/>\r
+<eng-data cg="192." f="308.91" m="347.1" t="0."/>\r
+<eng-data cg="192." f="419.24" m="329.865" t="0.1"/>\r
+<eng-data cg="192." f="441.3" m="319.681" t="0.15"/>\r
+<eng-data cg="192." f="397.17" m="309.758" t="0.2"/>\r
+<eng-data cg="192." f="375.11" m="291.479" t="0.3"/>\r
+<eng-data cg="192." f="353.04" m="286.308" t="0.33"/>\r
+<eng-data cg="192." f="330.98" m="96.8816" t="1.5"/>\r
+<eng-data cg="192." f="286.85" m="38.3871" t="1.9"/>\r
+<eng-data cg="192." f="165.49" m="27.6805" t="2."/>\r
+<eng-data cg="192." f="110.33" m="21.152" t="2.1"/>\r
+<eng-data cg="192." f="66.19" m="4.43954" t="2.5"/>\r
+<eng-data cg="192." f="22.07" m="1.30596" t="2.65"/>\r
+<eng-data cg="192." f="0." m="-0." t="2.9"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Ellis Mountain J330\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J330 38 433 0 0.407232 0.820736 EM\r
- 0.055 482.013\r
- 0.169 515.156\r
- 0.283 509.959\r
- 0.398 511.485\r
- 0.512 509.155\r
- 0.626 503.627\r
- 0.740 495.461\r
- 0.854 486.118\r
- 0.969 477.786\r
- 1.083 472.073\r
- 1.197 455.861\r
- 1.310 433.714\r
- 1.425 407.542\r
- 1.540 367.945\r
- 1.654 271.221\r
- 1.768 203.711\r
- 1.881 152.800\r
- 1.996 106.108\r
- 2.110 91.404\r
- 2.225 72.286\r
- 2.339 63.983\r
- 2.452 61.809\r
- 2.567 42.010\r
- 2.681 16.437\r
- 2.796 4.496\r
- 2.910 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="213.33" Itot="861.701" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="313.346" burn-time="2.75" cgDiv="10" cgFix="1" cgStep="-1." code="J330" delays="20,1000" dia="38." exitDia="0." initWt="780." len="433." mDiv="10" mFix="1" mStep="-1." massFrac="52.81" mfg="Ellis Mountain" peakThrust="541.77" propWt="411.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="216.5" f="0." m="411.9" t="0."/>\r
+<eng-data cg="216.5" f="541.77" m="405.426" t="0.05"/>\r
+<eng-data cg="216.5" f="520.1" m="400.35" t="0.07"/>\r
+<eng-data cg="216.5" f="485.43" m="369.108" t="0.2"/>\r
+<eng-data cg="216.5" f="507.1" m="297.942" t="0.5"/>\r
+<eng-data cg="216.5" f="455.09" m="182.958" t="1."/>\r
+<eng-data cg="216.5" f="433.42" m="129.869" t="1.25"/>\r
+<eng-data cg="216.5" f="379.24" m="81.3117" t="1.5"/>\r
+<eng-data cg="216.5" f="216.71" m="42.8544" t="1.77"/>\r
+<eng-data cg="216.5" f="104.02" m="25.2235" t="2."/>\r
+<eng-data cg="216.5" f="99.69" m="20.3548" t="2.1"/>\r
+<eng-data cg="216.5" f="86.68" m="15.9005" t="2.2"/>\r
+<eng-data cg="216.5" f="73.68" m="4.40245" t="2.5"/>\r
+<eng-data cg="216.5" f="0." m="-0." t="2.75"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-K475 54 663.6 14 1.035 2.168 Ellis_Mountain \r
-0.0463679 797.157\r
-0.15456 616.585\r
-0.278207 585.756\r
-0.479134 568.139\r
-2.92117 576.948\r
-3.29212 568.139\r
-4.00309 303.888\r
-4.51314 224.613\r
-5.02318 74.8711\r
-5.5 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="239.88" Itot="2434.77" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="442.686" burn-time="5.5" cgDiv="10" cgFix="1" cgStep="-1." code="K475" delays="14" dia="54." exitDia="0." initWt="2168." len="663.6" mDiv="10" mFix="1" mStep="-1." massFrac="47.74" mfg="Ellis Mountain" peakThrust="797.157" propWt="1035." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="331.8" f="0." m="1035." t="0."/>\r
+<eng-data cg="331.8" f="797.157" m="1027.14" t="0.0463679"/>\r
+<eng-data cg="331.8" f="616.585" m="994.634" t="0.15456"/>\r
+<eng-data cg="331.8" f="585.756" m="963.035" t="0.278207"/>\r
+<eng-data cg="331.8" f="568.139" m="913.757" t="0.479134"/>\r
+<eng-data cg="331.8" f="576.948" m="319.406" t="2.92117"/>\r
+<eng-data cg="331.8" f="568.139" m="229.123" t="3.29212"/>\r
+<eng-data cg="331.8" f="303.888" m="97.3482" t="4.00309"/>\r
+<eng-data cg="331.8" f="224.613" m="40.054" t="4.51314"/>\r
+<eng-data cg="331.8" f="74.8711" m="7.58789" t="5.02318"/>\r
+<eng-data cg="331.8" f="0." m="-0." t="5.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Ellis Mountain L330\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-L330 76 381 0 1.46944 2.67008 EM\r
- 0.194 298.963\r
- 0.584 378.807\r
- 0.975 376.204\r
- 1.366 382.475\r
- 1.757 391.163\r
- 2.148 399.442\r
- 2.539 406.048\r
- 2.930 407.731\r
- 3.321 405.666\r
- 3.711 400.636\r
- 4.103 393.384\r
- 4.494 384.520\r
- 4.884 377.009\r
- 5.275 368.385\r
- 5.666 359.041\r
- 6.057 350.117\r
- 6.448 341.587\r
- 6.839 337.109\r
- 7.230 300.039\r
- 7.621 194.602\r
- 8.011 123.445\r
- 8.403 66.942\r
- 8.794 32.233\r
- 9.184 8.248\r
- 9.576 1.563\r
- 9.968 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="199.2" Itot="2910.49" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="311.283" burn-time="9.35" cgDiv="10" cgFix="1" cgStep="-1." code="L330" delays="1000" dia="76." exitDia="0." initWt="2395.9" len="381." mDiv="10" mFix="1" mStep="-1." massFrac="62.19" mfg="Ellis Mountain" peakThrust="392.3" propWt="1489.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="190.5" f="0." m="1489.9" t="0."/>\r
+<eng-data cg="190.5" f="343." m="1485.51" t="0.05"/>\r
+<eng-data cg="190.5" f="381.58" m="1448.42" t="0.25"/>\r
+<eng-data cg="190.5" f="362.29" m="1400.82" t="0.5"/>\r
+<eng-data cg="190.5" f="360.15" m="1308.36" t="1."/>\r
+<eng-data cg="190.5" f="390.16" m="1020.3" t="2.5"/>\r
+<eng-data cg="190.5" f="392.3" m="820.025" t="3.5"/>\r
+<eng-data cg="190.5" f="325.85" m="268.587" t="6.5"/>\r
+<eng-data cg="190.5" f="321.56" m="102.88" t="7.5"/>\r
+<eng-data cg="190.5" f="317.27" m="86.5288" t="7.6"/>\r
+<eng-data cg="190.5" f="150.06" m="38.683" t="8."/>\r
+<eng-data cg="190.5" f="64.31" m="11.2486" t="8.5"/>\r
+<eng-data cg="190.5" f="21.44" m="2.46944" t="8.9"/>\r
+<eng-data cg="190.5" f="0." m="-0." t="9.35"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Ellis Mountain L600\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-L600 76 584 0 2.4407 4.11981 EM\r
- 0.186 829.668\r
- 0.561 773.861\r
- 0.936 767.837\r
- 1.313 755.034\r
- 1.689 736.454\r
- 2.064 722.717\r
- 2.440 706.215\r
- 2.816 688.253\r
- 3.191 673.457\r
- 3.567 660.981\r
- 3.943 648.124\r
- 4.318 634.689\r
- 4.694 622.058\r
- 5.070 607.970\r
- 5.445 594.926\r
- 5.821 583.003\r
- 6.197 573.084\r
- 6.572 553.530\r
- 6.948 399.379\r
- 7.324 270.410\r
- 7.699 211.401\r
- 8.075 144.237\r
- 8.451 74.227\r
- 8.826 19.378\r
- 9.202 4.274\r
- 9.578 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="204.75" Itot="4900.81" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="511.674" burn-time="9.58" cgDiv="10" cgFix="1" cgStep="-1." code="L600" delays="1000" dia="76." exitDia="0." initWt="4119.81" len="584." mDiv="10" mFix="1" mStep="-1." massFrac="59.24" mfg="Ellis Mountain" peakThrust="829.668" propWt="2440.7" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Ellis Mountain L600\r
+Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
+provided by ThrustCurve.org (www.thrustcurve.org)\r
+</comments>\r
+<data>\r
+<eng-data cg="292." f="0." m="2440.7" t="0."/>\r
+<eng-data cg="292." f="829.668" m="2402.27" t="0.186"/>\r
+<eng-data cg="292." f="773.861" m="2252.54" t="0.561"/>\r
+<eng-data cg="292." f="767.837" m="2108.58" t="0.936"/>\r
+<eng-data cg="292." f="755.034" m="1965.61" t="1.313"/>\r
+<eng-data cg="292." f="736.454" m="1825.97" t="1.689"/>\r
+<eng-data cg="292." f="722.717" m="1689.71" t="2.064"/>\r
+<eng-data cg="292." f="706.215" m="1555.93" t="2.44"/>\r
+<eng-data cg="292." f="688.253" m="1425.37" t="2.816"/>\r
+<eng-data cg="292." f="673.457" m="1298.21" t="3.191"/>\r
+<eng-data cg="292." f="660.981" m="1173.27" t="3.567"/>\r
+<eng-data cg="292." f="648.124" m="1050.7" t="3.943"/>\r
+<eng-data cg="292." f="634.689" m="930.914" t="4.318"/>\r
+<eng-data cg="292." f="622.058" m="813.248" t="4.694"/>\r
+<eng-data cg="292." f="607.97" m="698.083" t="5.07"/>\r
+<eng-data cg="292." f="594.926" m="585.758" t="5.445"/>\r
+<eng-data cg="292." f="583.003" m="475.471" t="5.821"/>\r
+<eng-data cg="292." f="573.084" m="367.229" t="6.197"/>\r
+<eng-data cg="292." f="553.53" m="262.028" t="6.572"/>\r
+<eng-data cg="292." f="399.379" m="172.809" t="6.948"/>\r
+<eng-data cg="292." f="270.41" m="110.098" t="7.324"/>\r
+<eng-data cg="292." f="211.401" m="65.1072" t="7.699"/>\r
+<eng-data cg="292." f="144.237" m="31.8097" t="8.075"/>\r
+<eng-data cg="292." f="74.227" m="11.3554" t="8.451"/>\r
+<eng-data cg="292." f="19.378" m="2.61465" t="8.826"/>\r
+<eng-data cg="292." f="4.274" m="0.400165" t="9.202"/>\r
+<eng-data cg="292." f="0." m="-0." t="9.578"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Ellis Mountain M1000\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-M1000 76 787 0 3.47514 5.5776 EM\r
- 0.159 1897.088\r
- 0.481 1606.200\r
- 0.803 1441.676\r
- 1.125 1360.014\r
- 1.447 1299.506\r
- 1.769 1259.449\r
- 2.091 1231.131\r
- 2.413 1202.529\r
- 2.735 1179.968\r
- 3.057 1154.573\r
- 3.379 1108.815\r
- 3.701 1075.453\r
- 4.023 1045.316\r
- 4.345 1010.304\r
- 4.667 951.184\r
- 4.989 860.548\r
- 5.310 727.369\r
- 5.633 595.659\r
- 5.955 518.911\r
- 6.277 439.902\r
- 6.599 347.743\r
- 6.921 239.388\r
- 7.243 144.608\r
- 7.565 75.112\r
- 7.887 33.539\r
- 8.210 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="211.01" Itot="7191.18" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="875.906" burn-time="8.21" cgDiv="10" cgFix="1" cgStep="-1." code="M1000" delays="1000" dia="75." exitDia="0." initWt="5577.6" len="787." mDiv="10" mFix="1" mStep="-1." massFrac="62.31" mfg="Ellis Mountain" peakThrust="1897.85" propWt="3475.14" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="393.5" f="0." m="3475.14" t="0."/>\r
+<eng-data cg="393.5" f="1897.85" m="3401.77" t="0.16"/>\r
+<eng-data cg="393.5" f="1606.84" m="3130.79" t="0.48"/>\r
+<eng-data cg="393.5" f="1442.25" m="2895.03" t="0.8"/>\r
+<eng-data cg="393.5" f="1360.56" m="2671.55" t="1.13"/>\r
+<eng-data cg="393.5" f="1300.03" m="2465.83" t="1.45"/>\r
+<eng-data cg="393.5" f="1259.95" m="2267.89" t="1.77"/>\r
+<eng-data cg="393.5" f="1231.62" m="2075.24" t="2.09"/>\r
+<eng-data cg="393.5" f="1203.01" m="1887." t="2.41"/>\r
+<eng-data cg="393.5" f="1180.44" m="1702.71" t="2.73"/>\r
+<eng-data cg="393.5" f="1155.04" m="1516.49" t="3.06"/>\r
+<eng-data cg="393.5" f="1109.26" m="1341.41" t="3.38"/>\r
+<eng-data cg="393.5" f="1075.88" m="1172.46" t="3.7"/>\r
+<eng-data cg="393.5" f="1045.73" m="1008.41" t="4.02"/>\r
+<eng-data cg="393.5" f="1010.71" m="849.409" t="4.34"/>\r
+<eng-data cg="393.5" f="951.57" m="692.944" t="4.67"/>\r
+<eng-data cg="393.5" f="860.89" m="552.804" t="4.99"/>\r
+<eng-data cg="393.5" f="727.66" m="429.978" t="5.31"/>\r
+<eng-data cg="393.5" f="595.9" m="327.64" t="5.63"/>\r
+<eng-data cg="393.5" f="519.12" m="238.732" t="5.96"/>\r
+<eng-data cg="393.5" f="440.08" m="164.567" t="6.28"/>\r
+<eng-data cg="393.5" f="347.88" m="103.642" t="6.6"/>\r
+<eng-data cg="393.5" f="239.48" m="58.2273" t="6.92"/>\r
+<eng-data cg="393.5" f="144.67" m="28.5248" t="7.24"/>\r
+<eng-data cg="393.5" f="75.14" m="10.998" t="7.57"/>\r
+<eng-data cg="393.5" f="33.55" m="2.59409" t="7.89"/>\r
+<eng-data cg="393.5" f="0." m="-0." t="8.21"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="55.64" Itot="1.091" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="3.031" burn-time="0.36" cgDiv="10" cgFix="1" cgStep="-1." code="1/2A3T" delays="2,4" dia="13." exitDia="0." initWt="6.6" len="45." mDiv="10" mFix="1" mStep="-1." massFrac="30.3" mfg="Estes" peakThrust="7.62" propWt="2." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <comments>Estes 1/2A3T RASP.ENG file made from NAR published data\r
+File produced October 3, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+ <data>\r
+ <eng-data cg="22.5" f="0." m="2." t="0."/>\r
+ <eng-data cg="22.5" f="0.501" m="1.98898" t="0.024"/>\r
+ <eng-data cg="22.5" f="1.454" m="1.95674" t="0.042"/>\r
+ <eng-data cg="22.5" f="3.009" m="1.86677" t="0.064"/>\r
+ <eng-data cg="22.5" f="4.062" m="1.78901" t="0.076"/>\r
+ <eng-data cg="22.5" f="4.914" m="1.69031" t="0.088"/>\r
+ <eng-data cg="22.5" f="5.065" m="1.64459" t="0.093"/>\r
+ <eng-data cg="22.5" f="6.068" m="1.54258" t="0.103"/>\r
+ <eng-data cg="22.5" f="6.87" m="1.43588" t="0.112"/>\r
+ <eng-data cg="22.5" f="7.021" m="1.37224" t="0.117"/>\r
+ <eng-data cg="22.5" f="7.62" m="1.25149" t="0.126"/>\r
+ <eng-data cg="22.5" f="7.472" m="1.09937" t="0.137"/>\r
+ <eng-data cg="22.5" f="6.87" m="0.981096" t="0.146"/>\r
+ <eng-data cg="22.5" f="6.118" m="0.897787" t="0.153"/>\r
+ <eng-data cg="22.5" f="5.065" m="0.836303" t="0.159"/>\r
+ <eng-data cg="22.5" f="4.363" m="0.77583" t="0.166"/>\r
+ <eng-data cg="22.5" f="3.66" m="0.680258" t="0.179"/>\r
+ <eng-data cg="22.5" f="2.908" m="0.571926" t="0.197"/>\r
+ <eng-data cg="22.5" f="2.256" m="0.453628" t="0.222"/>\r
+ <eng-data cg="22.5" f="2.156" m="0.340429" t="0.25"/>\r
+ <eng-data cg="22.5" f="2.106" m="0.234984" t="0.277"/>\r
+ <eng-data cg="22.5" f="2.056" m="0.17015" t="0.294"/>\r
+ <eng-data cg="22.5" f="2.156" m="0.131554" t="0.304"/>\r
+ <eng-data cg="22.5" f="1.955" m="0.08635" t="0.316"/>\r
+ <eng-data cg="22.5" f="1.554" m="0.0541961" t="0.326"/>\r
+ <eng-data cg="22.5" f="1.053" m="0.0231409" t="0.339"/>\r
+ <eng-data cg="22.5" f="0.651" m="0.00596528" t="0.35"/>\r
+ <eng-data cg="22.5" f="0." m="0." t="0.36"/>\r
+ </data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="44.31" Itot="1.13" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="3.424" burn-time="0.33" cgDiv="10" cgFix="1" cgStep="-1." code="1/2A6" delays="2" dia="18." exitDia="0." initWt="13.8" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="18.84" mfg="Estes" peakThrust="7.86" propWt="2.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Estes 1/2A6 RASP.ENG file made from NAR published data\r
+File produced October 3, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+ <eng-data cg="35." f="0." m="2.6" t="0."/>\r
+ <eng-data cg="35." f="0.404" m="2.58559" t="0.031"/>\r
+ <eng-data cg="35." f="1.258" m="2.52248" t="0.064"/>\r
+ <eng-data cg="35." f="2.263" m="2.39283" t="0.096"/>\r
+ <eng-data cg="35." f="3.467" m="2.20821" t="0.124"/>\r
+ <eng-data cg="35." f="4.72" m="1.9727" t="0.149"/>\r
+ <eng-data cg="35." f="6.023" m="1.68838" t="0.172"/>\r
+ <eng-data cg="35." f="7.027" m="1.32798" t="0.196"/>\r
+ <eng-data cg="35." f="7.528" m="1.09351" t="0.21"/>\r
+ <eng-data cg="35." f="7.86" m="0.827909" t="0.225"/>\r
+ <eng-data cg="35." f="7.482" m="0.651372" t="0.235"/>\r
+ <eng-data cg="35." f="6.683" m="0.504677" t="0.244"/>\r
+ <eng-data cg="35." f="5.685" m="0.362361" t="0.254"/>\r
+ <eng-data cg="35." f="4.487" m="0.257018" t="0.263"/>\r
+ <eng-data cg="35." f="4.087" m="0.197823" t="0.269"/>\r
+ <eng-data cg="35." f="3.039" m="0.115825" t="0.279"/>\r
+ <eng-data cg="35." f="1.79" m="0.0547022" t="0.29"/>\r
+ <eng-data cg="35." f="1.042" m="0.0318911" t="0.297"/>\r
+ <eng-data cg="35." f="0.593" m="0.0149589" t="0.306"/>\r
+ <eng-data cg="35." f="0.344" m="0.00633335" t="0.314"/>\r
+ <eng-data cg="35." f="0." m="0." t="0.33"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="72.46" Itot="0.59" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2.359" burn-time="0.25" cgDiv="10" cgFix="1" cgStep="-1." code="1/4A3T" delays="3" dia="13." exitDia="0." initWt="6.1" len="45." mDiv="10" mFix="1" mStep="-1." massFrac="13.61" mfg="Estes" peakThrust="4.95" propWt="0.83" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <comments>Estes 1/4A3T RASP.ENG file made from NAR published data\r
+File produced October 3, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+ <data>\r
+ <eng-data cg="22.5" f="0." m="0.83" t="0."/>\r
+ <eng-data cg="22.5" f="0.243" m="0.827264" t="0.016"/>\r
+ <eng-data cg="22.5" f="1.164" m="0.799545" t="0.044"/>\r
+ <eng-data cg="22.5" f="2.698" m="0.701722" t="0.08"/>\r
+ <eng-data cg="22.5" f="2.851" m="0.670487" t="0.088"/>\r
+ <eng-data cg="22.5" f="3.312" m="0.635797" t="0.096"/>\r
+ <eng-data cg="22.5" f="3.804" m="0.590735" t="0.105"/>\r
+ <eng-data cg="22.5" f="4.325" m="0.527819" t="0.116"/>\r
+ <eng-data cg="22.5" f="4.754" m="0.444775" t="0.129"/>\r
+ <eng-data cg="22.5" f="4.754" m="0.431395" t="0.131"/>\r
+ <eng-data cg="22.5" f="4.95" m="0.404084" t="0.135"/>\r
+ <eng-data cg="22.5" f="4.815" m="0.376601" t="0.139"/>\r
+ <eng-data cg="22.5" f="4.814" m="0.349501" t="0.143"/>\r
+ <eng-data cg="22.5" f="4.66" m="0.309505" t="0.149"/>\r
+ <eng-data cg="22.5" f="4.289" m="0.259133" t="0.157"/>\r
+ <eng-data cg="22.5" f="3.548" m="0.170906" t="0.173"/>\r
+ <eng-data cg="22.5" f="2.808" m="0.108297" t="0.187"/>\r
+ <eng-data cg="22.5" f="2.592" m="0.0817005" t="0.194"/>\r
+ <eng-data cg="22.5" f="2.13" m="0.0717332" t="0.197"/>\r
+ <eng-data cg="22.5" f="1.913" m="0.0575099" t="0.202"/>\r
+ <eng-data cg="22.5" f="1.512" m="0.0478705" t="0.206"/>\r
+ <eng-data cg="22.5" f="1.389" m="0.0335824" t="0.213"/>\r
+ <eng-data cg="22.5" f="1.112" m="0.0247838" t="0.218"/>\r
+ <eng-data cg="22.5" f="0.802" m="0.0126635" t="0.227"/>\r
+ <eng-data cg="22.5" f="0.493" m="0.00446297" t="0.236"/>\r
+ <eng-data cg="22.5" f="0.277" m="0.00175409" t="0.241"/>\r
+ <eng-data cg="22.5" f="0." m="0." t="0.25"/>\r
+ </data>\r
+ </engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Estes A10T RASP.ENG file made from NAR published data\r
-;File produced October 3, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-A10T 13 45 3-100 0.0038 0.00525 Estes \r
-0.026 0.478\r
-0.055 1.919\r
-0.093 4.513\r
-0.124 8.165\r
-0.146 10.956\r
-0.166 12.64\r
-0.179 11.046\r
-0.194 7.966\r
-0.203 6.042\r
-0.209 3.154\r
-0.225 1.421\r
-0.26 1.225\r
-0.333 1.41\r
-0.456 1.206\r
-0.575 1.195\r
-0.663 1.282\r
-0.76 1.273\r
-0.811 1.268\r
-0.828 0.689\r
-0.85 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="53.61" Itot="1.998" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2.35" burn-time="0.85" cgDiv="10" cgFix="1" cgStep="-1." code="A10T" delays="3,100" dia="13." exitDia="0." initWt="5.25" len="45." mDiv="10" mFix="1" mStep="-1." massFrac="72.38" mfg="Estes" peakThrust="12.64" propWt="3.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Estes A10T RASP.ENG file made from NAR published data\r
+File produced October 3, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="22.5" f="0." m="3.8" t="0."/>\r
+<eng-data cg="22.5" f="0.478" m="3.78818" t="0.026"/>\r
+<eng-data cg="22.5" f="1.919" m="3.72207" t="0.055"/>\r
+<eng-data cg="22.5" f="4.513" m="3.48963" t="0.093"/>\r
+<eng-data cg="22.5" f="8.165" m="3.11587" t="0.124"/>\r
+<eng-data cg="22.5" f="10.956" m="2.71582" t="0.146"/>\r
+<eng-data cg="22.5" f="12.64" m="2.26703" t="0.166"/>\r
+<eng-data cg="22.5" f="11.046" m="1.97419" t="0.179"/>\r
+<eng-data cg="22.5" f="7.966" m="1.70299" t="0.194"/>\r
+<eng-data cg="22.5" f="6.042" m="1.58309" t="0.203"/>\r
+<eng-data cg="22.5" f="3.154" m="1.53062" t="0.209"/>\r
+<eng-data cg="22.5" f="1.421" m="1.46101" t="0.225"/>\r
+<eng-data cg="22.5" f="1.225" m="1.37293" t="0.26"/>\r
+<eng-data cg="22.5" f="1.41" m="1.19" t="0.333"/>\r
+<eng-data cg="22.5" f="1.206" m="0.884002" t="0.456"/>\r
+<eng-data cg="22.5" f="1.195" m="0.612283" t="0.575"/>\r
+<eng-data cg="22.5" f="1.282" m="0.404987" t="0.663"/>\r
+<eng-data cg="22.5" f="1.273" m="0.169296" t="0.76"/>\r
+<eng-data cg="22.5" f="1.268" m="0.0460542" t="0.811"/>\r
+<eng-data cg="22.5" f="0.689" m="0.0144153" t="0.828"/>\r
+<eng-data cg="22.5" f="0." m="0." t="0.85"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Estes A3T RASP.ENG file made from NAR published data\r
-;File produced October 3, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-A3T 13 45 4 0.0033 0.0085 Estes \r
-0.024 0.195\r
-0.048 0.899\r
-0.086 2.658\r
-0.11 4.183\r
-0.14 5.83\r
-0.159 5.395\r
-0.18 4.301\r
-0.199 3.635\r
-0.215 2.736\r
-0.234 2.267\r
-0.258 2.15\r
-0.315 2.072\r
-0.441 1.993\r
-0.554 2.033\r
-0.605 2.072\r
-0.673 1.954\r
-0.764 1.954\r
-0.874 2.072\r
-0.931 2.15\r
-0.953 2.072\r
-0.966 1.719\r
-0.977 1.173\r
-0.993 0.547\r
-1.01 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="68.63" Itot="2.221" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="2.199" burn-time="1.01" cgDiv="10" cgFix="1" cgStep="-1." code="A3T" delays="4" dia="13." exitDia="0." initWt="8.5" len="45." mDiv="10" mFix="1" mStep="-1." massFrac="38.82" mfg="Estes" peakThrust="5.83" propWt="3.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Estes A3T RASP.ENG file made from NAR published data\r
+File produced October 3, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="22.5" f="0." m="3.3" t="0."/>\r
+<eng-data cg="22.5" f="0.195" m="3.29652" t="0.024"/>\r
+<eng-data cg="22.5" f="0.899" m="3.27702" t="0.048"/>\r
+<eng-data cg="22.5" f="2.658" m="3.17661" t="0.086"/>\r
+<eng-data cg="22.5" f="4.183" m="3.05464" t="0.11"/>\r
+<eng-data cg="22.5" f="5.83" m="2.83149" t="0.14"/>\r
+<eng-data cg="22.5" f="5.395" m="2.67305" t="0.159"/>\r
+<eng-data cg="22.5" f="4.301" m="2.52179" t="0.18"/>\r
+<eng-data cg="22.5" f="3.635" m="2.40977" t="0.199"/>\r
+<eng-data cg="22.5" f="2.736" m="2.33405" t="0.215"/>\r
+<eng-data cg="22.5" f="2.267" m="2.26343" t="0.234"/>\r
+<eng-data cg="22.5" f="2.15" m="2.18468" t="0.258"/>\r
+<eng-data cg="22.5" f="2.072" m="2.00591" t="0.315"/>\r
+<eng-data cg="22.5" f="1.993" m="1.62541" t="0.441"/>\r
+<eng-data cg="22.5" f="2.033" m="1.28745" t="0.554"/>\r
+<eng-data cg="22.5" f="2.072" m="1.13193" t="0.605"/>\r
+<eng-data cg="22.5" f="1.954" m="0.92855" t="0.673"/>\r
+<eng-data cg="22.5" f="1.954" m="0.664363" t="0.764"/>\r
+<eng-data cg="22.5" f="2.072" m="0.335373" t="0.874"/>\r
+<eng-data cg="22.5" f="2.15" m="0.156597" t="0.931"/>\r
+<eng-data cg="22.5" f="2.072" m="0.0875954" t="0.953"/>\r
+<eng-data cg="22.5" f="1.719" m="0.0509843" t="0.966"/>\r
+<eng-data cg="22.5" f="1.173" m="0.0273519" t="0.977"/>\r
+<eng-data cg="22.5" f="0.547" m="0.006908" t="0.993"/>\r
+<eng-data cg="22.5" f="0." m="0." t="1.01"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Estes A8 RASP.ENG file made from NAR published data\r
-;File produced October 3, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-A8 18 70 3-5 0.0033 0.01635 Estes \r
-0.041 0.512\r
-0.084 2.115\r
-0.127 4.358\r
-0.166 6.794\r
-0.192 8.588\r
-0.206 9.294\r
-0.226 9.73\r
-0.236 8.845\r
-0.247 7.179\r
-0.261 5.063\r
-0.277 3.717\r
-0.306 3.205\r
-0.351 2.884\r
-0.405 2.499\r
-0.467 2.371\r
-0.532 2.307\r
-0.589 2.371\r
-0.632 2.371\r
-0.652 2.243\r
-0.668 1.794\r
-0.684 1.153\r
-0.703 0.448\r
-0.73 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="71.7" Itot="2.32" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="3.178" burn-time="0.73" cgDiv="10" cgFix="1" cgStep="-1." code="A8" delays="3,5" dia="18." exitDia="0." initWt="16.35" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="20.18" mfg="Estes" peakThrust="9.73" propWt="3.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Estes A8 RASP.ENG file made from NAR published data\r
+File produced October 3, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="3.3" t="0."/>\r
+<eng-data cg="35." f="0.512" m="3.28507" t="0.041"/>\r
+<eng-data cg="35." f="2.115" m="3.20474" t="0.084"/>\r
+<eng-data cg="35." f="4.358" m="3.0068" t="0.127"/>\r
+<eng-data cg="35." f="6.794" m="2.6975" t="0.166"/>\r
+<eng-data cg="35." f="8.588" m="2.41309" t="0.192"/>\r
+<eng-data cg="35." f="9.294" m="2.23506" t="0.206"/>\r
+<eng-data cg="35." f="9.73" m="1.96448" t="0.226"/>\r
+<eng-data cg="35." f="8.845" m="1.83238" t="0.236"/>\r
+<eng-data cg="35." f="7.179" m="1.70703" t="0.247"/>\r
+<eng-data cg="35." f="5.063" m="1.58515" t="0.261"/>\r
+<eng-data cg="35." f="3.717" m="1.48525" t="0.277"/>\r
+<eng-data cg="35." f="3.205" m="1.3425" t="0.306"/>\r
+<eng-data cg="35." f="2.884" m="1.14764" t="0.351"/>\r
+<eng-data cg="35." f="2.499" m="0.94092" t="0.405"/>\r
+<eng-data cg="35." f="2.371" m="0.726196" t="0.467"/>\r
+<eng-data cg="35." f="2.307" m="0.509957" t="0.532"/>\r
+<eng-data cg="35." f="2.371" m="0.320333" t="0.589"/>\r
+<eng-data cg="35." f="2.371" m="0.175326" t="0.632"/>\r
+<eng-data cg="35." f="2.243" m="0.109701" t="0.652"/>\r
+<eng-data cg="35." f="1.794" m="0.0637665" t="0.668"/>\r
+<eng-data cg="35." f="1.153" m="0.0302344" t="0.684"/>\r
+<eng-data cg="35." f="0.448" m="0.00860204" t="0.703"/>\r
+<eng-data cg="35." f="0." m="0." t="0.73"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Estes B4 RASP.ENG file made from NAR published data\r
-;File produced October 3, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-B4 18 70 2-4 0.006 0.0189 Estes \r
-0.02 0.418\r
-0.04 1.673\r
-0.065 4.076\r
-0.085 6.69\r
-0.105 9.304\r
-0.119 11.496\r
-0.136 12.75\r
-0.153 11.916\r
-0.173 10.666\r
-0.187 9.304\r
-0.198 7.214\r
-0.207 5.645\r
-0.226 4.809\r
-0.258 4.182\r
-0.326 3.763\r
-0.422 3.554\r
-0.549 3.345\r
-0.665 3.345\r
-0.776 3.345\r
-0.863 3.345\r
-0.94 3.449\r
-0.991 3.449\r
-1.002 2.404\r
-1.01 1.254\r
-1.03 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="72.91" Itot="4.29" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="4.165" burn-time="1.03" cgDiv="10" cgFix="1" cgStep="-1." code="B4" delays="2,4" dia="18." exitDia="0." initWt="18.9" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="31.75" mfg="Estes" peakThrust="12.75" propWt="6." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Estes B4 RASP.ENG file made from NAR published data\r
+File produced October 3, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="6." t="0."/>\r
+<eng-data cg="35." f="0.418" m="5.99415" t="0.02"/>\r
+<eng-data cg="35." f="1.673" m="5.96491" t="0.04"/>\r
+<eng-data cg="35." f="4.076" m="5.8644" t="0.065"/>\r
+<eng-data cg="35." f="6.69" m="5.71383" t="0.085"/>\r
+<eng-data cg="35." f="9.304" m="5.49014" t="0.105"/>\r
+<eng-data cg="35." f="11.496" m="5.2865" t="0.119"/>\r
+<eng-data cg="35." f="12.75" m="4.99826" t="0.136"/>\r
+<eng-data cg="35." f="11.916" m="4.70503" t="0.153"/>\r
+<eng-data cg="35." f="10.666" m="4.38919" t="0.173"/>\r
+<eng-data cg="35." f="9.304" m="4.19368" t="0.187"/>\r
+<eng-data cg="35." f="7.214" m="4.06662" t="0.198"/>\r
+<eng-data cg="35." f="5.645" m="3.98569" t="0.207"/>\r
+<eng-data cg="35." f="4.809" m="3.84679" t="0.226"/>\r
+<eng-data cg="35." f="4.182" m="3.64559" t="0.258"/>\r
+<eng-data cg="35." f="3.763" m="3.26779" t="0.326"/>\r
+<eng-data cg="35." f="3.554" m="2.77658" t="0.422"/>\r
+<eng-data cg="35." f="3.345" m="2.16387" t="0.549"/>\r
+<eng-data cg="35." f="3.345" m="1.62118" t="0.665"/>\r
+<eng-data cg="35." f="3.345" m="1.10189" t="0.776"/>\r
+<eng-data cg="35." f="3.345" m="0.694871" t="0.863"/>\r
+<eng-data cg="35." f="3.449" m="0.329039" t="0.94"/>\r
+<eng-data cg="35." f="3.449" m="0.083026" t="0.991"/>\r
+<eng-data cg="35." f="2.404" m="0.0380029" t="1.002"/>\r
+<eng-data cg="35." f="1.254" m="0.0175385" t="1.01"/>\r
+<eng-data cg="35." f="0." m="0." t="1.03"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Estes B6-0 from NAR data by Mark Koelsch\r
-B6-0 18 70 0 0.0056 0.0156 E\r
- 0.036 1.364\r
- 0.064 2.727\r
- 0.082 4.215\r
- 0.111 6.694\r
- 0.135 9.05\r
- 0.146 9.545\r
- 0.172 11.901\r
- 0.181 12.149\r
- 0.191 11.901\r
- 0.211 9.174\r
- 0.239 7.314\r
- 0.264 6.074\r
- 0.275 5.95\r
- 0.333 5.207\r
- 0.394 4.835\r
- 0.445 4.835\r
- 0.556 4.339\r
- 0.667 4.587\r
- 0.723 4.339\r
- 0.78 4.339\r
- 0.793 4.091\r
- 0.812 2.603\r
- 0.833 1.24\r
- 0.857 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="78.81" Itot="4.328" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="5.033" burn-time="0.86" cgDiv="10" cgFix="1" cgStep="-1." code="B6" delays="0,2,4,6" dia="18." exitDia="0." initWt="18.22" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="30.74" mfg="Estes" peakThrust="12.14" propWt="5.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Estes B6 RASP.ENG file made from NAR published data\r
+File produced October 3, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="5.6" t="0."/>\r
+<eng-data cg="35." f="0.688" m="5.58976" t="0.023"/>\r
+<eng-data cg="35." f="2.457" m="5.52059" t="0.057"/>\r
+<eng-data cg="35." f="4.816" m="5.37002" t="0.089"/>\r
+<eng-data cg="35." f="7.274" m="5.15884" t="0.116"/>\r
+<eng-data cg="35." f="9.929" m="4.80271" t="0.148"/>\r
+<eng-data cg="35." f="12.14" m="4.47433" t="0.171"/>\r
+<eng-data cg="35." f="11.695" m="4.16594" t="0.191"/>\r
+<eng-data cg="35." f="10.719" m="4.03544" t="0.2"/>\r
+<eng-data cg="35." f="9.24" m="3.91923" t="0.209"/>\r
+<eng-data cg="35." f="7.667" m="3.68954" t="0.23"/>\r
+<eng-data cg="35." f="6.488" m="3.4606" t="0.255"/>\r
+<eng-data cg="35." f="5.505" m="3.07267" t="0.305"/>\r
+<eng-data cg="35." f="4.816" m="2.60528" t="0.375"/>\r
+<eng-data cg="35." f="4.62" m="1.98262" t="0.477"/>\r
+<eng-data cg="35." f="4.62" m="1.36692" t="0.58"/>\r
+<eng-data cg="35." f="4.521" m="0.828784" t="0.671"/>\r
+<eng-data cg="35." f="4.226" m="0.404379" t="0.746"/>\r
+<eng-data cg="35." f="4.325" m="0.183102" t="0.786"/>\r
+<eng-data cg="35." f="3.145" m="0.105781" t="0.802"/>\r
+<eng-data cg="35." f="1.572" m="0.0355943" t="0.825"/>\r
+<eng-data cg="35." f="0." m="0." t="0.86"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;ESTES C11 RASP.ENG file made from NAR published data\r
-;File produced JANUARY 1, 2002\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-C11 24 70 0-3-5-7 0.012 0.0353 Estes \r
-0.034 1.692\r
-0.066 3.782\r
-0.107 7.566\r
-0.145 10.946\r
-0.183 14.832\r
-0.214 17.618\r
-0.226 18.213\r
-0.256 20.107\r
-0.281 21.208\r
-0.298 21.73\r
-0.306 20.206\r
-0.323 17.321\r
-0.337 14.931\r
-0.358 13.236\r
-0.385 11.947\r
-0.413 11.65\r
-0.468 10.946\r
-0.539 10.45\r
-0.619 10.648\r
-0.683 10.648\r
-0.715 10.648\r
-0.726 10.053\r
-0.74 8.163\r
-0.758 5.773\r
-0.778 3.185\r
-0.795 1.394\r
-0.81 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="74.75" Itot="8.796" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="10.859" burn-time="0.81" cgDiv="10" cgFix="1" cgStep="-1." code="C11" delays="0,3,5,7" dia="24." exitDia="0." initWt="35.3" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="33.99" mfg="Estes" peakThrust="21.73" propWt="12." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>ESTES C11 RASP.ENG file made from NAR published data\r
+File produced JANUARY 1, 2002\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="12." t="0."/>\r
+<eng-data cg="35." f="1.692" m="11.9608" t="0.034"/>\r
+<eng-data cg="35." f="3.782" m="11.8413" t="0.066"/>\r
+<eng-data cg="35." f="7.566" m="11.5239" t="0.107"/>\r
+<eng-data cg="35." f="10.946" m="11.0441" t="0.145"/>\r
+<eng-data cg="35." f="14.832" m="10.3759" t="0.183"/>\r
+<eng-data cg="35." f="17.618" m="9.68969" t="0.214"/>\r
+<eng-data cg="35." f="18.213" m="9.3964" t="0.226"/>\r
+<eng-data cg="35." f="20.107" m="8.61223" t="0.256"/>\r
+<eng-data cg="35." f="21.208" m="7.90768" t="0.281"/>\r
+<eng-data cg="35." f="21.73" m="7.40977" t="0.298"/>\r
+<eng-data cg="35." f="20.206" m="7.18092" t="0.306"/>\r
+<eng-data cg="35." f="17.321" m="6.74575" t="0.323"/>\r
+<eng-data cg="35." f="14.931" m="6.43776" t="0.337"/>\r
+<eng-data cg="35." f="13.236" m="6.03428" t="0.358"/>\r
+<eng-data cg="35." f="11.947" m="5.57047" t="0.385"/>\r
+<eng-data cg="35." f="11.65" m="5.11978" t="0.413"/>\r
+<eng-data cg="35." f="10.946" m="4.27205" t="0.468"/>\r
+<eng-data cg="35." f="10.45" m="3.23583" t="0.539"/>\r
+<eng-data cg="35." f="10.648" m="2.08451" t="0.619"/>\r
+<eng-data cg="35." f="10.648" m="1.15481" t="0.683"/>\r
+<eng-data cg="35." f="10.648" m="0.689966" t="0.715"/>\r
+<eng-data cg="35." f="10.053" m="0.534638" t="0.726"/>\r
+<eng-data cg="35." f="8.163" m="0.36068" t="0.74"/>\r
+<eng-data cg="35." f="5.773" m="0.189571" t="0.758"/>\r
+<eng-data cg="35." f="3.185" m="0.0673618" t="0.778"/>\r
+<eng-data cg="35." f="1.394" m="0.0142632" t="0.795"/>\r
+<eng-data cg="35." f="0." m="0." t="0.81"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Estes C5 RASP.ENG file made from NAR published data\r
-;File produced October 3, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-C5 18 70 3 0.0113 0.0248 Estes \r
-0.042 2.195\r
-0.107 9.118\r
-0.159 16.213\r
-0.21 21.85\r
-0.233 18.407\r
-0.27 13.677\r
-0.289 9.793\r
-0.303 7.092\r
-0.326 5.065\r
-0.401 4.39\r
-0.55 3.883\r
-0.802 3.714\r
-1.026 3.883\r
-1.291 3.883\r
-1.524 4.221\r
-1.683 4.221\r
-1.702 2.195\r
-1.73 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="82.08" Itot="9.095" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="5.257" burn-time="1.73" cgDiv="10" cgFix="1" cgStep="-1." code="C5" delays="3" dia="18." exitDia="0." initWt="24.8" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="45.56" mfg="Estes" peakThrust="21.85" propWt="11.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Estes C5 RASP.ENG file made from NAR published data\r
+File produced October 3, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="11.3" t="0."/>\r
+<eng-data cg="35." f="2.195" m="11.2427" t="0.042"/>\r
+<eng-data cg="35." f="9.118" m="10.7859" t="0.107"/>\r
+<eng-data cg="35." f="16.213" m="9.96769" t="0.159"/>\r
+<eng-data cg="35." f="21.85" m="8.76182" t="0.21"/>\r
+<eng-data cg="35." f="18.407" m="8.18665" t="0.233"/>\r
+<eng-data cg="35." f="13.677" m="7.44923" t="0.27"/>\r
+<eng-data cg="35." f="9.793" m="7.17222" t="0.289"/>\r
+<eng-data cg="35." f="7.092" m="7.02537" t="0.303"/>\r
+<eng-data cg="35." f="5.065" m="6.85168" t="0.326"/>\r
+<eng-data cg="35." f="4.39" m="6.41117" t="0.401"/>\r
+<eng-data cg="35." f="3.883" m="5.64544" t="0.55"/>\r
+<eng-data cg="35." f="3.714" m="4.4562" t="0.802"/>\r
+<eng-data cg="35." f="3.883" m="3.39909" t="1.026"/>\r
+<eng-data cg="35." f="3.883" m="2.12068" t="1.291"/>\r
+<eng-data cg="35." f="4.221" m="0.947721" t="1.524"/>\r
+<eng-data cg="35." f="4.221" m="0.113905" t="1.683"/>\r
+<eng-data cg="35." f="2.195" m="0.0381786" t="1.702"/>\r
+<eng-data cg="35." f="0." m="0." t="1.73"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Estes C6 RASP.ENG file made from NAR published data\r
-;File produced October 3, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-C6 18 70 0-3-5-7 0.0108 0.0231 Estes \r
-0.031 0.946\r
-0.092 4.826\r
-0.139 9.936\r
-0.192 14.09\r
-0.209 11.446\r
-0.231 7.381\r
-0.248 6.151\r
-0.292 5.489\r
-0.37 4.921\r
-0.475 4.448\r
-0.671 4.258\r
-0.702 4.542\r
-0.723 4.164\r
-0.85 4.448\r
-1.063 4.353\r
-1.211 4.353\r
-1.242 4.069\r
-1.303 4.258\r
-1.468 4.353\r
-1.656 4.448\r
-1.821 4.448\r
-1.834 2.933\r
-1.847 1.325\r
-1.86 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="83.25" Itot="8.817" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="4.74" burn-time="1.86" cgDiv="10" cgFix="1" cgStep="-1." code="C6" delays="0,3,5,7" dia="18." exitDia="0." initWt="23.1" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="46.75" mfg="Estes" peakThrust="14.09" propWt="10.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Estes C6 RASP.ENG file made from NAR published data\r
+File produced October 3, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="10.8" t="0."/>\r
+<eng-data cg="35." f="0.946" m="10.782" t="0.031"/>\r
+<eng-data cg="35." f="4.826" m="10.5664" t="0.092"/>\r
+<eng-data cg="35." f="9.936" m="10.1415" t="0.139"/>\r
+<eng-data cg="35." f="14.09" m="9.36163" t="0.192"/>\r
+<eng-data cg="35." f="11.446" m="9.09576" t="0.209"/>\r
+<eng-data cg="35." f="7.381" m="8.84209" t="0.231"/>\r
+<eng-data cg="35." f="6.151" m="8.7012" t="0.248"/>\r
+<eng-data cg="35." f="5.489" m="8.38754" t="0.292"/>\r
+<eng-data cg="35." f="4.921" m="7.89025" t="0.37"/>\r
+<eng-data cg="35." f="4.448" m="7.28777" t="0.475"/>\r
+<eng-data cg="35." f="4.258" m="6.24272" t="0.671"/>\r
+<eng-data cg="35." f="4.542" m="6.07565" t="0.702"/>\r
+<eng-data cg="35." f="4.164" m="5.96368" t="0.723"/>\r
+<eng-data cg="35." f="4.448" m="5.29384" t="0.85"/>\r
+<eng-data cg="35." f="4.353" m="4.14576" t="1.063"/>\r
+<eng-data cg="35." f="4.353" m="3.35665" t="1.211"/>\r
+<eng-data cg="35." f="4.069" m="3.19675" t="1.242"/>\r
+<eng-data cg="35." f="4.258" m="2.88566" t="1.303"/>\r
+<eng-data cg="35." f="4.353" m="2.0155" t="1.468"/>\r
+<eng-data cg="35." f="4.448" m="1.00217" t="1.656"/>\r
+<eng-data cg="35." f="4.448" m="0.103215" t="1.821"/>\r
+<eng-data cg="35." f="2.933" m="0.04445" t="1.834"/>\r
+<eng-data cg="35." f="1.325" m="0.0105492" t="1.847"/>\r
+<eng-data cg="35." f="0." m="0." t="1.86"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Estes D11 RASP.ENG file made from NAR published data\r
-;File produced October 3, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-D11 24 70 100 0.0245 0.0448 Estes \r
-0.033 2.393\r
-0.084 5.783\r
-0.144 12.17\r
-0.214 20.757\r
-0.261 24.35\r
-0.289 26.01\r
-0.311 23.334\r
-0.325 18.532\r
-0.338 14.536\r
-0.356 12.331\r
-0.398 10.72\r
-0.48 9.303\r
-0.618 8.676\r
-0.761 8.247\r
-0.955 8.209\r
-1.222 7.955\r
-1.402 8.319\r
-1.54 8.291\r
-1.701 8.459\r
-1.784 8.442\r
-1.803 6.239\r
-1.834 3.033\r
-1.86 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="72.79" Itot="17.489" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="9.403" burn-time="1.86" cgDiv="10" cgFix="1" cgStep="-1." code="D11" delays="100" dia="24." exitDia="0." initWt="44.8" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="54.69" mfg="Estes" peakThrust="26.01" propWt="24.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Estes D11 RASP.ENG file made from NAR published data\r
+File produced October 3, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="24.5" t="0."/>\r
+<eng-data cg="35." f="2.393" m="24.4447" t="0.033"/>\r
+<eng-data cg="35." f="5.783" m="24.1526" t="0.084"/>\r
+<eng-data cg="35." f="12.17" m="23.3981" t="0.144"/>\r
+<eng-data cg="35." f="20.757" m="21.7838" t="0.214"/>\r
+<eng-data cg="35." f="24.35" m="20.2988" t="0.261"/>\r
+<eng-data cg="35." f="26.01" m="19.3112" t="0.289"/>\r
+<eng-data cg="35." f="23.334" m="18.5508" t="0.311"/>\r
+<eng-data cg="35." f="18.532" m="18.1403" t="0.325"/>\r
+<eng-data cg="35." f="14.536" m="17.8392" t="0.338"/>\r
+<eng-data cg="35." f="12.331" m="17.5005" t="0.356"/>\r
+<eng-data cg="35." f="10.72" m="16.8224" t="0.398"/>\r
+<eng-data cg="35." f="9.303" m="15.6724" t="0.48"/>\r
+<eng-data cg="35." f="8.676" m="13.9345" t="0.618"/>\r
+<eng-data cg="35." f="8.247" m="12.2395" t="0.761"/>\r
+<eng-data cg="35." f="8.209" m="10.0035" t="0.955"/>\r
+<eng-data cg="35." f="7.955" m="6.98058" t="1.222"/>\r
+<eng-data cg="35." f="8.319" m="4.92883" t="1.402"/>\r
+<eng-data cg="35." f="8.291" m="3.32333" t="1.54"/>\r
+<eng-data cg="35." f="8.459" m="1.43447" t="1.701"/>\r
+<eng-data cg="35." f="8.442" m="0.451932" t="1.784"/>\r
+<eng-data cg="35." f="6.239" m="0.256557" t="1.803"/>\r
+<eng-data cg="35." f="3.033" m="0.0552338" t="1.834"/>\r
+<eng-data cg="35." f="0." m="0." t="1.86"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Estes D12 RASP.ENG file made from NAR published data\r
-;File produced October 3, 2000\r
-;The total impulse, peak thrust, average thrust and burn time are\r
-;the same as the averaged static test data on the NAR web site in\r
-;the certification file. The curve drawn with these data points is as\r
-;close to the certification curve as can be with such a limited\r
-;number of points (32) allowed with wRASP up to v1.6.\r
-D12 24 70 0-3-5-7 0.0211 0.0426 Estes \r
-0.049 2.569\r
-0.116 9.369\r
-0.184 17.275\r
-0.237 24.258\r
-0.282 29.73\r
-0.297 27.01\r
-0.311 22.589\r
-0.322 17.99\r
-0.348 14.126\r
-0.386 12.099\r
-0.442 10.808\r
-0.546 9.876\r
-0.718 9.306\r
-0.879 9.105\r
-1.066 8.901\r
-1.257 8.698\r
-1.436 8.31\r
-1.59 8.294\r
-1.612 4.613\r
-1.65 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="81.38" Itot="16.839" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="10.206" burn-time="1.65" cgDiv="10" cgFix="1" cgStep="-1." code="D12" delays="0,3,5,7" dia="24." exitDia="0." initWt="42.6" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="49.53" mfg="Estes" peakThrust="29.73" propWt="21.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Estes D12 RASP.ENG file made from NAR published data\r
+File produced October 3, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="21.1" t="0."/>\r
+<eng-data cg="35." f="2.569" m="21.0211" t="0.049"/>\r
+<eng-data cg="35." f="9.369" m="20.52" t="0.116"/>\r
+<eng-data cg="35." f="17.275" m="19.3849" t="0.184"/>\r
+<eng-data cg="35." f="24.258" m="18.0058" t="0.237"/>\r
+<eng-data cg="35." f="29.73" m="16.4837" t="0.282"/>\r
+<eng-data cg="35." f="27.01" m="15.9505" t="0.297"/>\r
+<eng-data cg="35." f="22.589" m="15.5154" t="0.311"/>\r
+<eng-data cg="35." f="17.99" m="15.2358" t="0.322"/>\r
+<eng-data cg="35." f="14.126" m="14.7126" t="0.348"/>\r
+<eng-data cg="35." f="12.099" m="14.0882" t="0.386"/>\r
+<eng-data cg="35." f="10.808" m="13.2846" t="0.442"/>\r
+<eng-data cg="35." f="9.876" m="11.9368" t="0.546"/>\r
+<eng-data cg="35." f="9.306" m="9.86976" t="0.718"/>\r
+<eng-data cg="35." f="9.105" m="8.01266" t="0.879"/>\r
+<eng-data cg="35." f="8.901" m="5.9031" t="1.066"/>\r
+<eng-data cg="35." f="8.698" m="3.79713" t="1.257"/>\r
+<eng-data cg="35." f="8.31" m="1.88974" t="1.436"/>\r
+<eng-data cg="35." f="8.294" m="0.287726" t="1.59"/>\r
+<eng-data cg="35." f="4.613" m="0.109825" t="1.612"/>\r
+<eng-data cg="35." f="0." m="0." t="1.65"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Estes E9-0 by Mark Koelsch from NAR data\r
-E9-0 24 95 0 0.0358 0.056799999999999996 E\r
- 0.046 1.913\r
- 0.235 16.696\r
- 0.273 18.435\r
- 0.326 14.957\r
- 0.38 12.174\r
- 0.44 10.435\r
- 0.835 9.043\r
- 1.093 8.87\r
- 1.496 8.696\r
- 1.997 8.696\r
- 2.498 8.696\r
- 3.014 9.217\r
- 3.037 5.043\r
- 3.067 1.217\r
- 3.09 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="79.38" Itot="27.867" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="9.018" burn-time="3.09" cgDiv="10" cgFix="1" cgStep="-1." code="E9" delays="0,4,6,8,100" dia="24." exitDia="0." initWt="64.6" len="95." mDiv="10" mFix="1" mStep="-1." massFrac="55.42" mfg="Estes" peakThrust="19.47" propWt="35.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>ESTES E9 RASP.ENG file made from NAR published data\r
+File produced JANUARY 1, 2002\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="47.5" f="0." m="35.8" t="0."/>\r
+<eng-data cg="47.5" f="1.623" m="35.7593" t="0.039"/>\r
+<eng-data cg="47.5" f="5.36" m="35.544" t="0.087"/>\r
+<eng-data cg="47.5" f="9.746" m="35.0783" t="0.135"/>\r
+<eng-data cg="47.5" f="13.971" m="34.4232" t="0.178"/>\r
+<eng-data cg="47.5" f="16.81" m="33.6719" t="0.216"/>\r
+<eng-data cg="47.5" f="19.47" m="32.4368" t="0.269"/>\r
+<eng-data cg="47.5" f="17.141" m="31.7313" t="0.299"/>\r
+<eng-data cg="47.5" f="14.292" m="31.1255" t="0.329"/>\r
+<eng-data cg="47.5" f="12.427" m="30.5249" t="0.364"/>\r
+<eng-data cg="47.5" f="10.802" m="29.7937" t="0.413"/>\r
+<eng-data cg="47.5" f="9.989" m="28.5384" t="0.507"/>\r
+<eng-data cg="47.5" f="9.421" m="26.7679" t="0.649"/>\r
+<eng-data cg="47.5" f="8.852" m="24.8782" t="0.81"/>\r
+<eng-data cg="47.5" f="8.771" m="21.1653" t="1.138"/>\r
+<eng-data cg="47.5" f="8.527" m="20.7208" t="1.178"/>\r
+<eng-data cg="47.5" f="8.527" m="17.6645" t="1.457"/>\r
+<eng-data cg="47.5" f="8.608" m="16.3217" t="1.579"/>\r
+<eng-data cg="47.5" f="8.608" m="13.7783" t="1.809"/>\r
+<eng-data cg="47.5" f="8.527" m="11.1917" t="2.044"/>\r
+<eng-data cg="47.5" f="8.608" m="8.55019" t="2.284"/>\r
+<eng-data cg="47.5" f="8.689" m="6.16143" t="2.499"/>\r
+<eng-data cg="47.5" f="8.608" m="5.07259" t="2.597"/>\r
+<eng-data cg="47.5" f="9.014" m="3.79351" t="2.71"/>\r
+<eng-data cg="47.5" f="8.689" m="2.73598" t="2.803"/>\r
+<eng-data cg="47.5" f="9.096" m="1.73067" t="2.891"/>\r
+<eng-data cg="47.5" f="9.258" m="0.928979" t="2.959"/>\r
+<eng-data cg="47.5" f="9.339" m="0.343646" t="3.008"/>\r
+<eng-data cg="47.5" f="7.227" m="0.184031" t="3.023"/>\r
+<eng-data cg="47.5" f="4.466" m="0.101411" t="3.034"/>\r
+<eng-data cg="47.5" f="1.623" m="0.0427432" t="3.049"/>\r
+<eng-data cg="47.5" f="0." m="0." t="3.09"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; False data to test 1/2/4A-motors
-1/2A3 11 58 0-3-5-7 0.003 0.0067 Apogee
-0.014 0.241
-0.036 0.895
-0.064 2.618
-0.1 4.82
-0.111 4.133
-0.125 2.687
-0.139 2.307
-; More false data
-1/4A5 11 58 0-3-5-7 0.003 0.0067 Apogee
-0.014 0.241
-0.036 0.895
-0.064 2.618
-0.1 4.82
-0.111 4.133
-0.125 2.687
-0.139 2.307
--- /dev/null
+H186RT 38 248 18 0.1765 0.469 Gorilla_Rocket_Motors \r
+0.008 40.184\r
+0.042 133.634\r
+0.058 178\r
+0.1 196.9\r
+0.192 204\r
+0.483 215\r
+0.842 220.33\r
+1.075 219\r
+1.267 219\r
+1.35 207\r
+1.42 165\r
+1.48 118.949\r
+1.542 75\r
+1.69 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Gorilla_Rocket_Motors" code="H225BL" Type="reloadable" dia="38." len="248."\r
+initWt="475." propWt="182." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="241.149" peakThrust="305.169" throatDia="0." exitDia="0."\r
+Itot="313.493" burn-time="1.3" massFrac="38.32" Isp="175.65" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="182." cg="124."/>\r
+ <eng-data t="0.0150659" f="113.792" m="181.502" cg="124."/>\r
+ <eng-data t="0.0326428" f="193.101" m="179.937" cg="124."/>\r
+ <eng-data t="0.0489642" f="172.412" m="178.205" cg="124."/>\r
+ <eng-data t="0.166981" f="256.893" m="163.498" cg="124."/>\r
+ <eng-data t="0.310107" f="296.548" m="140.504" cg="124."/>\r
+ <eng-data t="0.512241" f="303.445" m="105.3" cg="124."/>\r
+ <eng-data t="0.617702" f="305.169" m="86.6684" cg="124."/>\r
+ <eng-data t="0.838669" f="298.272" m="47.9627" cg="124."/>\r
+ <eng-data t="0.898933" f="291.376" m="37.6479" cg="124."/>\r
+ <eng-data t="0.98" f="266.893" m="24.5108" cg="124."/>\r
+ <eng-data t="1.02" f="244.652" m="18.5712" cg="124."/>\r
+ <eng-data t="1.05" f="222.411" m="14.5038" cg="124."/>\r
+ <eng-data t="1.26303" f="10.3447" m="0.111027" cg="124."/>\r
+ <eng-data t="1.3" f="0." m="0." cg="124."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+I223GT 38 248 18 0.182 0.475 Gorilla_Rocket_Motors \r
+0.02 170\r
+0.05 190\r
+0.141038 225\r
+0.462292 255\r
+0.681685 258\r
+0.887365 260\r
+1.14789 255\r
+1.32419 224.138\r
+1.40451 129.31\r
+1.48 0\r
--- /dev/null
+I324RT 38 369 1000 0.298 0.688 Gorilla_Rocket_Motors \r
+0.015 238.506\r
+0.09 310\r
+0.25 360\r
+0.65 365\r
+1.06758 369.24\r
+1.25563 365\r
+1.35 340\r
+1.48678 195.402\r
+1.65 0\r
--- /dev/null
+I389GT 38 369 18 0.3026 0.6928 Gorilla_Rocket_Motors \r
+0.016 181.961\r
+0.025 277.057\r
+0.045 379.719\r
+0.065 413.405\r
+0.366 450\r
+0.683 454.85\r
+1.066 443.265\r
+1.14398 421\r
+1.183 385\r
+1.241 280.84\r
+1.35 92.872\r
+1.42 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="121.8" Itot="955.526" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="156.644" burn-time="6.1" cgDiv="10" cgFix="1" cgStep="-1." code="J167WC" delays="1000" dia="54." exitDia="0." initWt="1215.8" len="326." mDiv="10" mFix="1" mStep="-1." massFrac="65.8" mfg="Gorilla Motors" peakThrust="369.35" propWt="600." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="163." f="0." m="800." t="0."/>\r
+<eng-data cg="163." f="307.05" m="787.146" t="0.1"/>\r
+<eng-data cg="163." f="298.15" m="761.812" t="0.2"/>\r
+<eng-data cg="163." f="369.35" m="705.926" t="0.4"/>\r
+<eng-data cg="163." f="311.5" m="677.425" t="0.5"/>\r
+<eng-data cg="163." f="267." m="653.208" t="0.6"/>\r
+<eng-data cg="163." f="235.85" m="463.756" t="1.5"/>\r
+<eng-data cg="163." f="17.8" m="1.86285" t="5.85"/>\r
+<eng-data cg="163." f="0." m="0." t="6.1"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="176.32" Itot="861.074" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="361.796" burn-time="2.38" cgDiv="10" cgFix="1" cgStep="-1." code="J365BL" delays="1000" dia="54." exitDia="0." initWt="1204.54" len="326." mDiv="10" mFix="1" mStep="-1." massFrac="41.34" mfg="Gorilla Motors" peakThrust="498.4" propWt="498." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <data>\r
+ <eng-data cg="163." f="0." m="498." t="0."/>\r
+ <eng-data cg="163." f="102.35" m="496.816" t="0.04"/>\r
+ <eng-data cg="163." f="155.75" m="495.323" t="0.06"/>\r
+ <eng-data cg="163." f="192.8" m="491.292" t="0.1"/>\r
+ <eng-data cg="163." f="242.308" m="483.796" t="0.159574"/>\r
+ <eng-data cg="163." f="315.95" m="444.983" t="0.4"/>\r
+ <eng-data cg="163." f="400.5" m="403.548" t="0.6"/>\r
+ <eng-data cg="163." f="436.1" m="379.355" t="0.7"/>\r
+ <eng-data cg="163." f="480.6" m="331.64" t="0.88"/>\r
+ <eng-data cg="163." f="498.4" m="246.71" t="1.18"/>\r
+ <eng-data cg="163." f="445." m="132.131" t="1.6"/>\r
+ <eng-data cg="163." f="378.25" m="25.003" t="2.05"/>\r
+ <eng-data cg="163." f="213.6" m="9.5997" t="2.14"/>\r
+ <eng-data cg="163." f="102.35" m="4.11783" t="2.2"/>\r
+ <eng-data cg="163." f="22.25" m="0.514729" t="2.3"/>\r
+ <eng-data cg="163." f="0." m="0." t="2.38"/>\r
+ </data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+J395RT 54 326 1000 0.5406 1.1604 Gorilla_Rocket_Motors \r
+0.06 267\r
+0.1 333.75\r
+0.16 356\r
+0.21 360.45\r
+0.33 387.15\r
+1 460.157\r
+1.5 453.9\r
+2.2 409.4\r
+2.4 360.45\r
+2.48 267\r
+2.57 44.5\r
+2.59 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="173.88" Itot="1122.02" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="436.584" burn-time="2.57" cgDiv="10" cgFix="1" cgStep="-1." code="J450BL" delays="1000" dia="54." exitDia="0." initWt="1454.54" len="430." mDiv="10" mFix="1" mStep="-1." massFrac="45.24" mfg="Gorilla Motors" peakThrust="601." propWt="658." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+ <eng-data cg="215." f="0." m="658." t="0."/>\r
+ <eng-data cg="215." f="124.6" m="655.077" t="0.08"/>\r
+ <eng-data cg="215." f="333.75" m="640.293" t="0.19"/>\r
+ <eng-data cg="215." f="413.85" m="616.18" t="0.3"/>\r
+ <eng-data cg="215." f="556.25" m="508.088" t="0.68"/>\r
+ <eng-data cg="215." f="578.5" m="468.16" t="0.8"/>\r
+ <eng-data cg="215." f="601." m="381.696" t="1.05"/>\r
+ <eng-data cg="215." f="547.35" m="233.539" t="1.49"/>\r
+ <eng-data cg="215." f="409.4" m="34.3563" t="2.2"/>\r
+ <eng-data cg="215." f="267." m="14.5228" t="2.3"/>\r
+ <eng-data cg="215." f="84.55" m="4.21461" t="2.4"/>\r
+ <eng-data cg="215." f="0." m="0." t="2.57"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="187.86" Itot="1042.75" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="465.514" burn-time="2.24" cgDiv="10" cgFix="1" cgStep="-1." code="J465GT" delays="1000" dia="54." exitDia="0." initWt="1181.8" len="326." mDiv="10" mFix="1" mStep="-1." massFrac="47.89" mfg="Gorilla Motors" peakThrust="662.6" propWt="566." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <data>\r
+ <eng-data cg="163." f="0." m="566." t="0."/>\r
+ <eng-data cg="163." f="364.9" m="557.087" t="0.09"/>\r
+ <eng-data cg="163." f="382.7" m="555.058" t="0.1"/>\r
+ <eng-data cg="163." f="400.5" m="546.556" t="0.14"/>\r
+ <eng-data cg="163." f="662.6" m="252.263" t="1.16"/>\r
+ <eng-data cg="163." f="650." m="213.077" t="1.27"/>\r
+ <eng-data cg="163." f="338.2" m="17.2945" t="2."/>\r
+ <eng-data cg="163." f="231.4" m="9.56513" t="2.05"/>\r
+ <eng-data cg="163." f="124.6" m="4.73426" t="2.1"/>\r
+ <eng-data cg="163." f="0." m="0." t="2.24"/>\r
+ </data>\r
+ </engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Gorilla_Rocket_Motors" code="J485WC" Type="reloadable" dia="54." len="326."\r
+initWt="1164.8" propWt="549." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="492.077" peakThrust="573.821" throatDia="0." exitDia="0."\r
+Itot="1077.65" burn-time="2.19" massFrac="47.13" Isp="200.16" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="549." cg="163."/>\r
+ <eng-data t="0.05" f="263.913" m="545.639" cg="163."/>\r
+ <eng-data t="0.095" f="401.808" m="538.008" cg="163."/>\r
+ <eng-data t="0.15" f="444.822" m="526.147" cg="163."/>\r
+ <eng-data t="0.503226" f="544.253" m="437.156" cg="163."/>\r
+ <eng-data t="0.8" f="573.821" m="352.635" cg="163."/>\r
+ <eng-data t="1.075" f="569.372" m="272.557" cg="163."/>\r
+ <eng-data t="1.5" f="542.683" m="152.169" cg="163."/>\r
+ <eng-data t="2." f="444.822" m="26.4002" cg="163."/>\r
+ <eng-data t="2.1" f="311.376" m="7.13827" cg="163."/>\r
+ <eng-data t="2.19" f="0." m="0." cg="163."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Gorilla_Rocket_Motors" code="K1075RT" Type="reloadable" dia="54."\r
+len="728." initWt="2541." propWt="1314." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="1075.06" peakThrust="1247.2" throatDia="0."\r
+exitDia="0." Itot="2408.12" burn-time="2.24" massFrac="51.71" Isp="186.88"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="1314." cg="364."/>\r
+ <eng-data t="0.017" f="687.71" m="1310.81" cg="364."/>\r
+ <eng-data t="0.042" f="1026.66" m="1299.12" cg="364."/>\r
+ <eng-data t="0.134" f="1121.18" m="1245.21" cg="364."/>\r
+ <eng-data t="0.242" f="1171.15" m="1177.66" cg="364."/>\r
+ <eng-data t="0.325" f="1203.77" m="1123.88" cg="364."/>\r
+ <eng-data t="1.225" f="1247.2" m="522.062" cg="364."/>\r
+ <eng-data t="1.659" f="1238.53" m="227.735" cg="364."/>\r
+ <eng-data t="1.742" f="1223.36" m="171.987" cg="364."/>\r
+ <eng-data t="1.8" f="1123.36" m="134.852" cg="364."/>\r
+ <eng-data t="2.24" f="0." m="0." cg="364."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+K1185GT 54 728 1000 1.314 2.541 Gorilla_Rocket_Motors \r
+0.01 575\r
+0.06 810\r
+0.12 1050\r
+0.17 1175\r
+0.68 1345\r
+0.82 1366.15\r
+0.92 1379\r
+1.65 1290.5\r
+1.8 1268.25\r
+1.85 1223.75\r
+1.87 1068\r
+1.92 801\r
+2.05 222.5\r
+2.1 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="165.47" Itot="1298.15" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="196.689" burn-time="6.6" cgDiv="10" cgFix="1" cgStep="-1." code="K222WC" delays="1000" dia="54." exitDia="0." initWt="1596.54" len="430." mDiv="10" mFix="1" mStep="-1." massFrac="50.11" mfg="Gorilla Motors" peakThrust="422.75" propWt="800." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="215." f="0." m="800." t="0."/>\r
+<eng-data cg="215." f="400.5" m="787.659" t="0.1"/>\r
+<eng-data cg="215." f="378.25" m="775.661" t="0.15"/>\r
+<eng-data cg="215." f="422.75" m="713.958" t="0.4"/>\r
+<eng-data cg="215." f="347.1" m="690.237" t="0.5"/>\r
+<eng-data cg="215." f="289.25" m="562.785" t="1.15"/>\r
+<eng-data cg="215." f="267." m="374.247" t="2.25"/>\r
+<eng-data cg="215." f="231.4" m="259.068" t="3."/>\r
+<eng-data cg="215." f="169.1" m="135.661" t="4."/>\r
+<eng-data cg="215." f="44.5" m="8.1414" t="5.9375"/>\r
+<eng-data cg="215." f="22.25" m="2.74237" t="6.2"/>\r
+<eng-data cg="215." f="0." m="0." t="6.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="166.57" Itot="1633.52" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="297.003" burn-time="5.5" cgDiv="10" cgFix="1" cgStep="-1." code="K327WC" delays="1000" dia="54." exitDia="0." initWt="1816.7" len="492." mDiv="10" mFix="1" mStep="-1." massFrac="55.04" mfg="Gorilla Motors" peakThrust="684.54" propWt="1000." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="246." f="0." m="1000." t="0."/>\r
+<eng-data cg="246." f="556.25" m="991.487" t="0.05"/>\r
+<eng-data cg="246." f="520.65" m="958.524" t="0.15"/>\r
+<eng-data cg="246." f="684.54" m="829.411" t="0.5"/>\r
+<eng-data cg="246." f="534." m="773.464" t="0.65"/>\r
+<eng-data cg="246." f="22.25" m="2.17935" t="5.18"/>\r
+<eng-data cg="246." f="0." m="0." t="5.5"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Gorilla_Rocket_Motors" code="K470WC" Type="reloadable" dia="54." len="728."\r
+initWt="2327." propWt="1400." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="464.469" peakThrust="1050.2" throatDia="0." exitDia="0."\r
+Itot="2450.07" burn-time="5.28" massFrac="60.16" Isp="178.46" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="1400." cg="364."/>\r
+ <eng-data t="0.025" f="1001.25" m="1392.85" cg="364."/>\r
+ <eng-data t="0.175" f="905." m="1311.15" cg="364."/>\r
+ <eng-data t="0.45" f="1050.2" m="1157.54" cg="364."/>\r
+ <eng-data t="0.65" f="827.7" m="1050.23" cg="364."/>\r
+ <eng-data t="1.091" f="716.45" m="855.674" cg="364."/>\r
+ <eng-data t="1.633" f="623." m="648.257" cg="364."/>\r
+ <eng-data t="5.275" f="0." m="0." cg="364."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+K520RT 54 430 1000 0.7211 1.4421 Gorilla_Rocket_Motors \r
+0.05 400.5\r
+0.07 471.7\r
+0.16 502.85\r
+0.23 498.4\r
+0.35 529.55\r
+0.87 593.13\r
+1.2 605.2\r
+1.55 578.5\r
+1.85 569.6\r
+2.32 511.75\r
+2.45 387.15\r
+2.58 26.7\r
+2.61 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="162.51" Itot="1434.35" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="531.239" burn-time="2.7" cgDiv="10" cgFix="1" cgStep="-1." code="K533BL" delays="1000" dia="54." exitDia="0." initWt="1716.7" len="492." mDiv="10" mFix="1" mStep="-1." massFrac="52.43" mfg="Gorilla Motors" peakThrust="694.2" propWt="900." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="246." f="0." m="900." t="0."/>\r
+<eng-data cg="246." f="467.25" m="885.341" t="0.1"/>\r
+<eng-data cg="246." f="694.2" m="648.491" t="0.75"/>\r
+<eng-data cg="246." f="680.85" m="454.363" t="1.2"/>\r
+<eng-data cg="246." f="631.9" m="310.215" t="1.55"/>\r
+<eng-data cg="246." f="489.5" m="63.9417" t="2.25"/>\r
+<eng-data cg="246." f="17.8" m="0.279221" t="2.65"/>\r
+<eng-data cg="246." f="0." m="0." t="2.7"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Gorilla_Rocket_Motors" code="K630WC" Type="reloadable" dia="54." len="430."\r
+initWt="1453.3" propWt="732." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="632.417" peakThrust="800.68" throatDia="0." exitDia="0."\r
+Itot="1416.61" burn-time="2.24" massFrac="50.37" Isp="197.34" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="732." cg="215."/>\r
+ <eng-data t="0.042" f="359.461" m="728.099" cg="215."/>\r
+ <eng-data t="0.05" f="440.908" m="726.445" cg="215."/>\r
+ <eng-data t="0.075" f="556.028" m="720.006" cg="215."/>\r
+ <eng-data t="0.15" f="622.751" m="697.164" cg="215."/>\r
+ <eng-data t="0.217" f="667.233" m="674.834" cg="215."/>\r
+ <eng-data t="0.9" f="800.68" m="415.804" cg="215."/>\r
+ <eng-data t="1.159" f="796.232" m="308.945" cg="215."/>\r
+ <eng-data t="1.33871" f="778.439" m="235.833" cg="215."/>\r
+ <eng-data t="1.517" f="720.612" m="166.781" cg="215."/>\r
+ <eng-data t="1.9" f="556.028" m="40.4538" cg="215."/>\r
+ <eng-data t="2.1" f="133.447" m="4.82688" cg="215."/>\r
+ <eng-data t="2.24" f="0." m="0." cg="215."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+K700RT 54 492 1000 0.90135 1.7535 Gorilla_Rocket_Motors \r
+0.12 534\r
+0.18 658.6\r
+0.2 725.35\r
+0.24 747.6\r
+0.28 747.6\r
+0.4 783.2\r
+0.65 788.215\r
+1 787.65\r
+1.65 769.85\r
+2 729.8\r
+2.1 712\r
+2.2 645.25\r
+2.38 115.7\r
+2.41 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Gorilla_Motors" code="K763GT" Type="reloadable" dia="54." len="492."\r
+initWt="1810." propWt="954." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="760.078" peakThrust="867.75" throatDia="0." exitDia="0."\r
+Itot="1725.38" burn-time="2.27" massFrac="52.71" Isp="184.42" tDiv="6"\r
+tStep="-1." tFix="1" FDiv="6" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1"\r
+cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments><![CDATA[The K763GT "Green Tornado" motor is a green flame, low smoke propellant.\r
+This reload produces a 36% "K" motor with 1740.27 N-seconds of total impulse,\r
+maximum thrust of 867.75 Newtons, and an average thrust of 763.56 Newtons,\r
+for a 2.27 second burn time.\r
+]]></comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="954." cg="246."/>\r
+ <eng-data t="0.05" f="498.4" m="947.111" cg="246."/>\r
+ <eng-data t="0.07" f="565.15" m="941.23" cg="246."/>\r
+ <eng-data t="0.08" f="623." m="937.945" cg="246."/>\r
+ <eng-data t="0.1" f="689.75" m="930.687" cg="246."/>\r
+ <eng-data t="0.12" f="720.9" m="922.887" cg="246."/>\r
+ <eng-data t="0.25" f="801." m="868.19" cg="246."/>\r
+ <eng-data t="0.38" f="845.5" m="809.015" cg="246."/>\r
+ <eng-data t="0.65" f="867.75" m="681.13" cg="246."/>\r
+ <eng-data t="0.83" f="854.4" m="595.43" cg="246."/>\r
+ <eng-data t="1.95" f="778.75" m="89.747" cg="246."/>\r
+ <eng-data t="2.1" f="712." m="27.9268" cg="246."/>\r
+ <eng-data t="2.15" f="400.5" m="12.5486" cg="246."/>\r
+ <eng-data t="2.25" f="44.5" m="0.246051" cg="246."/>\r
+ <eng-data t="2.27" f="0." m="0." cg="246."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Gorilla_Rocket_Motors" code="K805WC" Type="reloadable" dia="54." len="492."\r
+initWt="1739.65" propWt="887.5" delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="811.365" peakThrust="1089.81" throatDia="0." exitDia="0."\r
+Itot="1776.89" burn-time="2.19" massFrac="51.02" Isp="204.16" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="887.5" cg="246."/>\r
+ <eng-data t="0.025" f="423.515" m="884.856" cg="246."/>\r
+ <eng-data t="0.0403226" f="667.233" m="880.682" cg="246."/>\r
+ <eng-data t="0.067" f="702.819" m="871.554" cg="246."/>\r
+ <eng-data t="0.095" f="747.301" m="861.414" cg="246."/>\r
+ <eng-data t="0.551613" f="1000.85" m="662.069" cg="246."/>\r
+ <eng-data t="0.8" f="1089.81" m="532.384" cg="246."/>\r
+ <eng-data t="1.25" f="1067.57" m="289.937" cg="246."/>\r
+ <eng-data t="1.75" f="667.233" m="73.3176" cg="246."/>\r
+ <eng-data t="2.19" f="0." m="0." cg="246."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Gorilla_Rocket_Motors" code="K980BL" Type="reloadable" dia="54." len="728."\r
+initWt="2457." propWt="1230." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="981.525" peakThrust="1297.45" throatDia="0." exitDia="0."\r
+Itot="2129.91" burn-time="2.17" massFrac="50.06" Isp="176.58" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="1230." cg="364."/>\r
+ <eng-data t="0.05" f="1186.45" m="1212.87" cg="364."/>\r
+ <eng-data t="0.07" f="1021.76" m="1200.12" cg="364."/>\r
+ <eng-data t="0.25" f="1135.45" m="1088." cg="364."/>\r
+ <eng-data t="0.35" f="1200." m="1020.56" cg="364."/>\r
+ <eng-data t="0.5" f="1225.45" m="915.514" cg="364."/>\r
+ <eng-data t="0.75" f="1297.45" m="733.396" cg="364."/>\r
+ <eng-data t="0.91" f="1265.75" m="614.978" cg="364."/>\r
+ <eng-data t="1.1" f="1201.5" m="479.621" cg="364."/>\r
+ <eng-data t="1.58" f="1045.75" m="168.158" cg="364."/>\r
+ <eng-data t="1.65" f="1068." m="125.434" cg="364."/>\r
+ <eng-data t="1.7" f="1001.25" m="95.5601" cg="364."/>\r
+ <eng-data t="1.8" f="495." m="52.3567" cg="364."/>\r
+ <eng-data t="2." f="222.5" m="10.9218" cg="364."/>\r
+ <eng-data t="2.17" f="0." m="0." cg="364."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+L1065BL 75 787 1000 2.693 5.329 Gorilla_Rocket_Motors \r
+0.02 1334.47\r
+0.1 1312.23\r
+0.65 1779.29\r
+1.75 1757.05\r
+2.2 1245.5\r
+2.75 667.233\r
+3.5 222.411\r
+3.95 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Gorilla Rocket Motors" code="L1150WC" Type="reloadable" dia="75."\r
+len="497." initWt="3502." propWt="1750." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="1148.98" peakThrust="1757.05" throatDia="0."\r
+exitDia="0." Itot="3573.33" burn-time="3.11" massFrac="49.97" Isp="208.22"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="1750." cg="248.5"/>\r
+ <eng-data t="0.1" f="1000.85" m="1725.49" cg="248.5"/>\r
+ <eng-data t="0.2" f="1067.57" m="1674.84" cg="248.5"/>\r
+ <eng-data t="0.5" f="1178.78" m="1509.82" cg="248.5"/>\r
+ <eng-data t="1.25" f="1668.08" m="986.99" cg="248.5"/>\r
+ <eng-data t="1.5" f="1757.05" m="777.312" cg="248.5"/>\r
+ <eng-data t="1.7" f="1734.81" m="606.302" cg="248.5"/>\r
+ <eng-data t="2." f="1334.47" m="380.831" cg="248.5"/>\r
+ <eng-data t="2.25047" f="982.747" m="238.71" cg="248.5"/>\r
+ <eng-data t="2.5" f="711.716" m="135.174" cg="248.5"/>\r
+ <eng-data t="2.75" f="556.028" m="57.5661" cg="248.5"/>\r
+ <eng-data t="3." f="266.893" m="7.18896" cg="248.5"/>\r
+ <eng-data t="3.11" f="0." m="0." cg="248.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Gorilla_Rocket_Motors" code="L425WC" Type="reloadable" dia="75." len="497."\r
+initWt="3502." propWt="1750." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="424.572" peakThrust="756.198" throatDia="0." exitDia="0."\r
+Itot="3375.35" burn-time="7.95" massFrac="49.97" Isp="196.68" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="1750." cg="248.5"/>\r
+ <eng-data t="0.02" f="756.198" m="1746.08" cg="248.5"/>\r
+ <eng-data t="0.05" f="711.716" m="1734.66" cg="248.5"/>\r
+ <eng-data t="0.125" f="756.198" m="1706.12" cg="248.5"/>\r
+ <eng-data t="0.180791" f="689.647" m="1685.21" cg="248.5"/>\r
+ <eng-data t="0.361582" f="662.061" m="1621.86" cg="248.5"/>\r
+ <eng-data t="0.514124" f="644.82" m="1570.18" cg="248.5"/>\r
+ <eng-data t="0.954802" f="631.027" m="1424.43" cg="248.5"/>\r
+ <eng-data t="1.28249" f="620.682" m="1318.1" cg="248.5"/>\r
+ <eng-data t="2.00565" f="586.2" m="1091.85" cg="248.5"/>\r
+ <eng-data t="2.96296" f="524.132" m="816.306" cg="248.5"/>\r
+ <eng-data t="4.42561" f="427.581" m="455.448" cg="248.5"/>\r
+ <eng-data t="5.46139" f="341.375" m="248.977" cg="248.5"/>\r
+ <eng-data t="6.5725" f="224.135" m="86.0895" cg="248.5"/>\r
+ <eng-data t="7.37602" f="110.343" m="16.4185" cg="248.5"/>\r
+ <eng-data t="7.95" f="0." m="0." cg="248.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Gorilla_Rocket_Motors" code="L695BL" Type="reloadable" dia="75." len="497."\r
+initWt="3402." propWt="1650." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="698.531" peakThrust="1064.64" throatDia="0." exitDia="0."\r
+Itot="2682.36" burn-time="3.84" massFrac="48.5" Isp="165.77" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="1650." cg="248.5"/>\r
+ <eng-data t="0.01" f="333.617" m="1648.97" cg="248.5"/>\r
+ <eng-data t="0.05" f="378.099" m="1640.22" cg="248.5"/>\r
+ <eng-data t="0.49592" f="560.338" m="1511.51" cg="248.5"/>\r
+ <eng-data t="0.994978" f="724.129" m="1314.36" cg="248.5"/>\r
+ <eng-data t="1.49718" f="883.61" m="1066.03" cg="248.5"/>\r
+ <eng-data t="1.98996" f="1043.09" m="774.012" cg="248.5"/>\r
+ <eng-data t="2.1312" f="1064.64" m="682.449" cg="248.5"/>\r
+ <eng-data t="2.2693" f="1064.64" m="592.006" cg="248.5"/>\r
+ <eng-data t="2.50471" f="1064.64" m="437.841" cg="248.5"/>\r
+ <eng-data t="2.63967" f="1043.09" m="350.347" cg="248.5"/>\r
+ <eng-data t="2.76208" f="965.506" m="274.725" cg="248.5"/>\r
+ <eng-data t="2.95355" f="797.404" m="170.912" cg="248.5"/>\r
+ <eng-data t="3.1764" f="512.925" m="81.1013" cg="248.5"/>\r
+ <eng-data t="3.36472" f="288.79" m="34.6645" cg="248.5"/>\r
+ <eng-data t="3.69115" f="38.7926" m="1.77598" cg="248.5"/>\r
+ <eng-data t="3.84" f="0." m="0." cg="248.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+L789RT 75 497 1000 1.8 3.378 Gorilla_Rocket_Motors \r
+0.05 600\r
+0.1 650\r
+0.2 712\r
+0.754163 850\r
+1.5 900\r
+2 906\r
+3.41332 867.816\r
+3.55 833.333\r
+3.92752 344.828\r
+4.17 0\r
--- /dev/null
+L985GT 75 497 1000 1.875 3.453 Gorilla_Rocket_Motors \r
+0.2 725\r
+0.3 795.5\r
+0.75 950\r
+1.5 1120\r
+2 1120\r
+3.4 1112.5\r
+3.6 0\r
--- /dev/null
+M1355RT 75 787 1000 2.831 5.216 Gorilla_Rocket_Motors_ \r
+0.05 1334.47\r
+0.85 1779.29\r
+1.35 1868.25\r
+1.7 1890.49\r
+2.15 1859.36\r
+3.5 489.304\r
+3.81 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Gorilla_Rocket_Motors" code="M1610BL" Type="reloadable" dia="75."\r
+len="1039." initWt="6918." propWt="3674." delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="1613.68" peakThrust="2206.87" throatDia="0."\r
+exitDia="0." Itot="5986.77" burn-time="3.71" massFrac="53.11" Isp="166.16"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="3674." cg="519.5"/>\r
+ <eng-data t="0.0627746" f="1560.33" m="3643.95" cg="519.5"/>\r
+ <eng-data t="1.3" f="2135.15" m="2241.02" cg="519.5"/>\r
+ <eng-data t="1.64783" f="2206.87" m="1777.59" cg="519.5"/>\r
+ <eng-data t="1.79535" f="2206.87" m="1577.8" cg="519.5"/>\r
+ <eng-data t="1.89893" f="2189.63" m="1438.07" cg="519.5"/>\r
+ <eng-data t="1.98996" f="2155.15" m="1316.72" cg="519.5"/>\r
+ <eng-data t="2.50157" f="1715.5" m="709.085" cg="519.5"/>\r
+ <eng-data t="2.82486" f="1474.12" m="392.677" cg="519.5"/>\r
+ <eng-data t="2.99435" f="1241.36" m="251.452" cg="519.5"/>\r
+ <eng-data t="3.29253" f="594.82" m="83.4515" cg="519.5"/>\r
+ <eng-data t="3.5" f="355.858" m="22.9305" cg="519.5"/>\r
+ <eng-data t="3.71" f="0." m="0." cg="519.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+M1665WC 75 787 1000 2.95 5.579 Gorilla_Rocket_Motors \r
+0.075 2068.42\r
+0.125 2001.7\r
+0.7 2224.11\r
+0.85 2268.59\r
+1.6 2268.59\r
+2.12 1801.53\r
+2.65 1178.78\r
+3.22 444.822\r
+3.42 0\r
; HyperTek I310\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
+; converted from TMT test stand data 1998 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
I310 54 645 0 0.40096 1.30502 HT\r
0.042 465.886\r
; HyperTek J115 (440CC076J)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
J115 54 614 0 0.411264 1.28218 HT\r
0.129 218.303\r
; HyperTek J120 (440CC076JFX)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
J120 54 614 0 0.442176 1.29338 HT\r
0.134 232.707\r
; HyperTek J150\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
+; converted from TMT test stand data 1998 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
J150 54 645 0 0.428288 1.30592 HT\r
0.111 177.498\r
; HyperTek J170 (440CC098J)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
J170 54 614 0 0.4032 1.28218 HT\r
0.092 315.198\r
; HyperTek J190 (440CC098JFX)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
J190 54 614 0 0.439488 1.29338 HT\r
0.095 338.583\r
; HyperTek J220\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
+; converted from TMT test stand data 1998 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
J220 54 645 0 0.417984 1.30502 HT\r
0.071 277.975\r
; HyperTek J250 (440CC125J)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
J250 54 614 0 0.40768 1.29248 HT\r
0.064 409.711\r
+++ /dev/null
-; HyperTek J250\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-J250 54 645 0 0.404992 1.30637 HT\r
- 0.055 356.092\r
- 0.168 316.638\r
- 0.281 357.597\r
- 0.395 351.765\r
- 0.508 354.216\r
- 0.622 354.162\r
- 0.735 338.625\r
- 0.849 332.051\r
- 0.963 323.651\r
- 1.076 315.678\r
- 1.190 305.773\r
- 1.303 298.769\r
- 1.417 288.922\r
- 1.530 293.337\r
- 1.644 276.552\r
- 1.757 269.543\r
- 1.871 223.360\r
- 1.984 131.511\r
- 2.098 98.246\r
- 2.211 76.331\r
- 2.325 60.095\r
- 2.439 47.691\r
- 2.552 36.215\r
- 2.666 26.693\r
- 2.779 20.007\r
- 2.893 0.000\r
; HyperTek J270 (440CC125JFX)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
J270 54 614 0 0.419776 1.29606 HT\r
0.064 438.643\r
; HyperTek J317O (835CC172J)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
J317O 81 552 0 0.704256 1.7575 HT\r
0.071 438.483\r
; HyperTek J330O (835CC172JFX)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
J330O 81 552 0 0.727104 1.77722 HT\r
0.068 453.500\r
; HyperTek K240\r
-; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)\r
+; converted from TMT test stand data 1998 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
K240 81 552 0 0.789376 1.80723 HT\r
0.131 278.007\r
; HyperTek L200 (1685CC098L)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
L200 111 724 0 1.59398 3.89491 HT\r
0.292 310.935\r
; HyperTek L225 (1685CC098LFX)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
L225 111 724 0 1.66118 3.94822 HT\r
0.271 380.609\r
; HyperTek L350 (1685CC125L)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
L350 111 724 0 1.6025 3.90342 HT\r
0.188 592.182\r
; HyperTek L355 (1685CC125LFX)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
L355 111 724 0 1.61952 3.95405 HT\r
0.185 638.681\r
; HyperTek L475 (1685CC172L)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
L475 111 724 0 1.52992 3.89805 HT\r
0.129 640.755\r
; HyperTek L535 (1685CC172LFX)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
L535 111 724 0 1.59667 3.94822 HT\r
0.119 838.518\r
; HyperTek L540O (2800CC172L)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
L540O 111 876 0 2.5303 5.656 HT\r
0.191 685.548\r
; HyperTek L550 (1685CCRGL)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
L550 111 724 0 1.53261 3.89805 HT\r
0.124 816.849\r
; HyperTek L570O (2800CC172LFX)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
L570O 111 876 0 2.57734 5.70618 HT\r
0.181 793.916\r
; HyperTek L575O (2800CCRGL)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
L575O 111 876 0 2.52134 5.65286 HT\r
0.190 705.343\r
; HyperTek L610 (1685CCRGLFX)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
L610 111 724 0 1.57696 3.95091 HT\r
0.110 850.823\r
; HyperTek L625O (2800CCRGLFX)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
L625O 111 876 0 2.56614 5.70618 HT\r
0.169 855.024\r
; HyperTek M1000O (4630CCRGM)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
M1000O 111 1147 0 4.17446 8.90714 HT\r
0.197 1368.441\r
; HyperTek M1010O (4630CCRGMFX)\r
-; Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+; converted from TMT test stand data 2001 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
M1010O 111 1147 0 4.27571 8.99987 HT\r
0.199 1473.475\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Kosdon-by-Aerotech" code="G135R" Type="reloadable" dia="29." len="206."\r
+initWt="226." propWt="80." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="136.999" peakThrust="158.178" throatDia="0." exitDia="0."\r
+Itot="143.712" burn-time="1.05" massFrac="35.4" Isp="183.18" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve and engine data TRA certification dated Oct 14,\r
+2008.\r
+</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="80." cg="103."/>\r
+ <eng-data t="0.011" f="156.916" m="79.5196" cg="103."/>\r
+ <eng-data t="0.016" f="63.461" m="79.2129" cg="103."/>\r
+ <eng-data t="0.027" f="98.191" m="78.718" cg="103."/>\r
+ <eng-data t="0.061" f="109.872" m="76.749" cg="103."/>\r
+ <eng-data t="0.094" f="111.135" m="74.719" cg="103."/>\r
+ <eng-data t="0.14" f="116.187" m="71.8085" cg="103."/>\r
+ <eng-data t="0.197" f="127.553" m="67.9415" cg="103."/>\r
+ <eng-data t="0.26" f="135.13" m="63.3354" cg="103."/>\r
+ <eng-data t="0.316" f="139.235" m="59.0589" cg="103."/>\r
+ <eng-data t="0.354" f="141.445" m="56.0902" cg="103."/>\r
+ <eng-data t="0.408" f="147.128" m="51.7529" cg="103."/>\r
+ <eng-data t="0.459" f="149.022" m="47.5491" cg="103."/>\r
+ <eng-data t="0.502" f="153.443" m="43.929" cg="103."/>\r
+ <eng-data t="0.546" f="156.6" m="40.132" cg="103."/>\r
+ <eng-data t="0.6" f="158.178" m="35.4009" cg="103."/>\r
+ <eng-data t="0.684" f="155.968" m="28.0561" cg="103."/>\r
+ <eng-data t="0.743" f="152.811" m="22.9854" cg="103."/>\r
+ <eng-data t="0.816" f="149.97" m="16.8334" cg="103."/>\r
+ <eng-data t="0.875" f="148.075" m="11.9389" cg="103."/>\r
+ <eng-data t="0.91" f="146.812" m="9.06622" cg="103."/>\r
+ <eng-data t="0.963" f="151.232" m="4.66954" cg="103."/>\r
+ <eng-data t="0.981" f="152.18" m="3.14944" cg="103."/>\r
+ <eng-data t="0.993" f="149.022" m="2.14342" cg="103."/>\r
+ <eng-data t="1.014" f="103.558" m="0.667078" cg="103."/>\r
+ <eng-data t="1.02" f="61.251" m="0.391845" cg="103."/>\r
+ <eng-data t="1.034" f="22.732" m="0.0645891" cg="103."/>\r
+ <eng-data t="1.039" f="7.893" m="0.021969" cg="103."/>\r
+ <eng-data t="1.049" f="0." m="0." cg="103."/>\r
+ </data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Kosdon-by-Aerotech" code="G82W" Type="reloadable" dia="29." len="206."\r
+initWt="231." propWt="84." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="73.433" peakThrust="103.839" throatDia="0." exitDia="0."\r
+Itot="143.856" burn-time="1.96" massFrac="36.36" Isp="174.63" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve and engine data TRA certification dated Oct 14,\r
+2008.\r
+</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="84." cg="103."/>\r
+ <eng-data t="0.011" f="50.341" m="83.8383" cg="103."/>\r
+ <eng-data t="0.028" f="53.498" m="83.3229" cg="103."/>\r
+ <eng-data t="0.055" f="76.3" m="82.2998" cg="103."/>\r
+ <eng-data t="0.068" f="80.159" m="81.7059" cg="103."/>\r
+ <eng-data t="0.111" f="74.02" m="79.7703" cg="103."/>\r
+ <eng-data t="0.134" f="74.02" m="78.7762" cg="103."/>\r
+ <eng-data t="0.216" f="79.458" m="75.1019" cg="103."/>\r
+ <eng-data t="0.295" f="83.667" m="71.3394" cg="103."/>\r
+ <eng-data t="0.374" f="89.982" m="67.3342" cg="103."/>\r
+ <eng-data t="0.406" f="91.911" m="65.6349" cg="103."/>\r
+ <eng-data t="0.431" f="89.631" m="64.3098" cg="103."/>\r
+ <eng-data t="0.453" f="92.437" m="63.1403" cg="103."/>\r
+ <eng-data t="0.474" f="93.841" m="61.9982" cg="103."/>\r
+ <eng-data t="0.489" f="91.385" m="61.1871" cg="103."/>\r
+ <eng-data t="0.519" f="93.314" m="59.5693" cg="103."/>\r
+ <eng-data t="0.551" f="90.333" m="57.8536" cg="103."/>\r
+ <eng-data t="0.604" f="91.911" m="55.0335" cg="103."/>\r
+ <eng-data t="0.642" f="92.262" m="52.9902" cg="103."/>\r
+ <eng-data t="0.728" f="94.367" m="48.3043" cg="103."/>\r
+ <eng-data t="0.79" f="96.647" m="44.8466" cg="103."/>\r
+ <eng-data t="0.85" f="98.401" m="41.4299" cg="103."/>\r
+ <eng-data t="0.905" f="99.453" m="38.2528" cg="103."/>\r
+ <eng-data t="0.954" f="101.734" m="35.3746" cg="103."/>\r
+ <eng-data t="0.995" f="102.962" m="32.9243" cg="103."/>\r
+ <eng-data t="1.025" f="103.839" m="31.113" cg="103."/>\r
+ <eng-data t="1.076" f="102.435" m="28.0416" cg="103."/>\r
+ <eng-data t="1.112" f="102.435" m="25.8883" cg="103."/>\r
+ <eng-data t="1.142" f="102.26" m="24.0954" cg="103."/>\r
+ <eng-data t="1.174" f="98.576" m="22.219" cg="103."/>\r
+ <eng-data t="1.221" f="95.244" m="19.5594" cg="103."/>\r
+ <eng-data t="1.238" f="93.49" m="18.6227" cg="103."/>\r
+ <eng-data t="1.274" f="98.226" m="16.6076" cg="103."/>\r
+ <eng-data t="1.287" f="89.631" m="15.8946" cg="103."/>\r
+ <eng-data t="1.317" f="87.877" m="14.3399" cg="103."/>\r
+ <eng-data t="1.351" f="85.597" m="12.6179" cg="103."/>\r
+ <eng-data t="1.434" f="81.913" m="8.55867" cg="103."/>\r
+ <eng-data t="1.479" f="78.581" m="6.45007" cg="103."/>\r
+ <eng-data t="1.503" f="73.845" m="5.38202" cg="103."/>\r
+ <eng-data t="1.533" f="65.075" m="4.16525" cg="103."/>\r
+ <eng-data t="1.565" f="50.516" m="3.08531" cg="103."/>\r
+ <eng-data t="1.594" f="36.835" m="2.34573" cg="103."/>\r
+ <eng-data t="1.62" f="28.591" m="1.84908" cg="103."/>\r
+ <eng-data t="1.65" f="21.048" m="1.4143" cg="103."/>\r
+ <eng-data t="1.701" f="14.208" m="0.889345" cg="103."/>\r
+ <eng-data t="1.737" f="8.946" m="0.645984" cg="103."/>\r
+ <eng-data t="1.829" f="5.613" m="0.254925" cg="103."/>\r
+ <eng-data t="1.883" f="4.385" m="0.0972984" cg="103."/>\r
+ <eng-data t="1.959" f="0." m="0." cg="103."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-Aerotech" code="H130W" Type="reloadable" dia="29." len="291."\r
+initWt="709." propWt="140." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="129.807" peakThrust="227.027" throatDia="0." exitDia="0."\r
+Itot="247.802" burn-time="1.91" massFrac="19.75" Isp="180.49" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve and engine data TRA certification dated Oct 14,\r
+2008.\r
+</comments>\r
+<data>\r
+ <eng-data t="0." f="0." m="140." cg="145.5"/>\r
+ <eng-data t="0.016" f="154.848" m="139.3" cg="145.5"/>\r
+ <eng-data t="0.024" f="194.715" m="138.51" cg="145.5"/>\r
+ <eng-data t="0.055" f="224.09" m="134.843" cg="145.5"/>\r
+ <eng-data t="0.071" f="201.848" m="132.918" cg="145.5"/>\r
+ <eng-data t="0.078" f="227.027" m="132.07" cg="145.5"/>\r
+ <eng-data t="0.089" f="183.384" m="130.794" cg="145.5"/>\r
+ <eng-data t="0.123" f="172.054" m="127.38" cg="145.5"/>\r
+ <eng-data t="0.196" f="172.054" m="120.285" cg="145.5"/>\r
+ <eng-data t="0.254" f="176.67" m="114.571" cg="145.5"/>\r
+ <eng-data t="0.348" f="179.607" m="105.111" cg="145.5"/>\r
+ <eng-data t="0.426" f="180.866" m="97.1681" cg="145.5"/>\r
+ <eng-data t="0.481" f="179.188" m="91.5741" cg="145.5"/>\r
+ <eng-data t="0.554" f="178.348" m="84.2012" cg="145.5"/>\r
+ <eng-data t="0.649" f="166.179" m="74.9555" cg="145.5"/>\r
+ <eng-data t="0.672" f="165.339" m="72.8016" cg="145.5"/>\r
+ <eng-data t="0.777" f="172.473" m="62.7819" cg="145.5"/>\r
+ <eng-data t="0.86" f="172.893" m="54.6844" cg="145.5"/>\r
+ <eng-data t="0.947" f="171.634" m="46.2173" cg="145.5"/>\r
+ <eng-data t="1.038" f="167.018" m="37.5119" cg="145.5"/>\r
+ <eng-data t="1.138" f="161.143" m="28.2419" cg="145.5"/>\r
+ <eng-data t="1.185" f="157.366" m="24.0131" cg="145.5"/>\r
+ <eng-data t="1.232" f="152.75" m="19.8958" cg="145.5"/>\r
+ <eng-data t="1.266" f="143.098" m="17.0544" cg="145.5"/>\r
+ <eng-data t="1.294" f="119.598" m="14.9766" cg="145.5"/>\r
+ <eng-data t="1.326" f="101.134" m="12.9813" cg="145.5"/>\r
+ <eng-data t="1.412" f="70.08" m="8.82188" cg="145.5"/>\r
+ <eng-data t="1.53" f="46.58" m="4.93325" cg="145.5"/>\r
+ <eng-data t="1.647" f="32.732" m="2.31194" cg="145.5"/>\r
+ <eng-data t="1.674" f="29.375" m="1.83825" cg="145.5"/>\r
+ <eng-data t="1.718" f="17.625" m="1.25408" cg="145.5"/>\r
+ <eng-data t="1.838" f="12.17" m="0.244085" cg="145.5"/>\r
+ <eng-data t="1.909" f="0." m="0." cg="145.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-Aerotech" code="H225R" Type="reloadable" dia="29." len="291."\r
+initWt="316." propWt="133." delays="10" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="216.545" peakThrust="275.523" throatDia="0." exitDia="0."\r
+Itot="242.747" burn-time="1.12" massFrac="42.09" Isp="186.12" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve and engine data TRA certification dated Oct 14,\r
+2008.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="133." cg="145.5"/>\r
+<eng-data t="0.025" f="104.61" m="132.284" cg="145.5"/>\r
+<eng-data t="0.039" f="112.468" m="131.451" cg="145.5"/>\r
+<eng-data t="0.053" f="123.764" m="130.545" cg="145.5"/>\r
+<eng-data t="0.091" f="141.936" m="127.779" cg="145.5"/>\r
+<eng-data t="0.104" f="177.297" m="126.642" cg="145.5"/>\r
+<eng-data t="0.131" f="189.576" m="123.929" cg="145.5"/>\r
+<eng-data t="0.16" f="195.96" m="120.866" cg="145.5"/>\r
+<eng-data t="0.26" f="219.534" m="109.483" cg="145.5"/>\r
+<eng-data t="0.336" f="229.848" m="100.127" cg="145.5"/>\r
+<eng-data t="0.345" f="225.919" m="99.0034" cg="145.5"/>\r
+<eng-data t="0.385" f="237.706" m="93.9231" cg="145.5"/>\r
+<eng-data t="0.43" f="251.949" m="87.8868" cg="145.5"/>\r
+<eng-data t="0.491" f="260.789" m="79.3185" cg="145.5"/>\r
+<eng-data t="0.527" f="264.718" m="74.1359" cg="145.5"/>\r
+<eng-data t="0.562" f="267.174" m="69.036" cg="145.5"/>\r
+<eng-data t="0.623" f="271.103" m="60.041" cg="145.5"/>\r
+<eng-data t="0.668" f="268.156" m="53.3932" cg="145.5"/>\r
+<eng-data t="0.713" f="269.629" m="46.7636" cg="145.5"/>\r
+<eng-data t="0.742" f="268.156" m="42.4911" cg="145.5"/>\r
+<eng-data t="0.794" f="262.754" m="34.9282" cg="145.5"/>\r
+<eng-data t="0.818" f="262.263" m="31.4763" cg="145.5"/>\r
+<eng-data t="0.855" f="259.316" m="26.1896" cg="145.5"/>\r
+<eng-data t="0.891" f="258.825" m="21.0796" cg="145.5"/>\r
+<eng-data t="0.927" f="263.736" m="15.926" cg="145.5"/>\r
+<eng-data t="0.957" f="272.576" m="11.5184" cg="145.5"/>\r
+<eng-data t="0.971" f="275.523" m="9.41629" cg="145.5"/>\r
+<eng-data t="0.982" f="271.594" m="7.76759" cg="145.5"/>\r
+<eng-data t="0.991" f="230.339" m="6.53006" cg="145.5"/>\r
+<eng-data t="1.008" f="185.647" m="4.59277" cg="145.5"/>\r
+<eng-data t="1.025" f="162.072" m="2.9734" cg="145.5"/>\r
+<eng-data t="1.055" f="72.687" m="1.04405" cg="145.5"/>\r
+<eng-data t="1.078" f="32.414" m="0.381829" cg="145.5"/>\r
+<eng-data t="1.121" f="0." m="0." cg="145.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;Data entered by Tim Van Milligan\r
-;Based on TRA Certification 6-19-2002\r
-;And Instructions provided by Aerotech.\r
-I170S 38 258 14 0.1819 0.52 Kosdon-by-Aerotech \r
-0.019 194.885\r
-0.131 190.481\r
-0.255 191.582\r
-0.513 199.289\r
-0.641 204.794\r
-0.753 206.996\r
-0.88 209.199\r
-1 208.098\r
-1.051 208.098\r
-1.147 206.996\r
-1.24 201.491\r
-1.391 198.188\r
-1.537 190.481\r
-1.707 181.672\r
-1.746 178.369\r
-1.781 173.96\r
-1.808 168.46\r
-1.854 132.12\r
-1.939 53.951\r
-2.005 22.02\r
-2.059 9.909\r
-2.13 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-Aerotech" code="I170S" Type="reloadable" dia="38." len="258."\r
+initWt="520." propWt="181.9" delays="14" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="175.585" peakThrust="209.199" throatDia="0." exitDia="0."\r
+Itot="373.995" burn-time="2.13" massFrac="34.98" Isp="209.66" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Data entered by Tim Van Milligan\r
+Based on TRA Certification 6-19-2002\r
+And Instructions provided by Aerotech.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="181.9" cg="129."/>\r
+<eng-data t="0.019" f="194.885" m="181." cg="129."/>\r
+<eng-data t="0.131" f="190.481" m="170.503" cg="129."/>\r
+<eng-data t="0.255" f="191.582" m="158.982" cg="129."/>\r
+<eng-data t="0.513" f="199.289" m="134.458" cg="129."/>\r
+<eng-data t="0.641" f="204.794" m="121.88" cg="129."/>\r
+<eng-data t="0.753" f="206.996" m="110.664" cg="129."/>\r
+<eng-data t="0.88" f="209.199" m="97.8105" cg="129."/>\r
+<eng-data t="1." f="208.098" m="85.6328" cg="129."/>\r
+<eng-data t="1.051" f="208.098" m="80.471" cg="129."/>\r
+<eng-data t="1.147" f="206.996" m="70.7803" cg="129."/>\r
+<eng-data t="1.24" f="201.491" m="61.5419" cg="129."/>\r
+<eng-data t="1.391" f="198.188" m="46.8653" cg="129."/>\r
+<eng-data t="1.537" f="190.481" m="33.0656" cg="129."/>\r
+<eng-data t="1.707" f="181.672" m="17.6803" cg="129."/>\r
+<eng-data t="1.746" f="178.369" m="14.2656" cg="129."/>\r
+<eng-data t="1.781" f="173.96" m="11.2667" cg="129."/>\r
+<eng-data t="1.808" f="168.46" m="9.01839" cg="129."/>\r
+<eng-data t="1.854" f="132.12" m="5.65595" cg="129."/>\r
+<eng-data t="1.939" f="53.951" m="1.80973" cg="129."/>\r
+<eng-data t="2.005" f="22.02" m="0.590381" cg="129."/>\r
+<eng-data t="2.059" f="9.909" m="0.17109" cg="129."/>\r
+<eng-data t="2.13" f="0." m="0." cg="129."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-I280F 38 258 14 100.182 0.52 Kosdon-by-AeroTech \r
-0.009 253.24\r
-0.055 255.442\r
-0.219 277.463\r
-0.482 301.686\r
-0.67 323.707\r
-0.735 330.314\r
-0.797 323.707\r
-1.001 297.282\r
-1.162 266.453\r
-1.205 259.847\r
-1.236 237.826\r
-1.363 50.6481\r
-1.428 26.4251\r
-1.5 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-AeroTech" code="I280F" Type="reloadable" dia="38." len="258."\r
+initWt="520." propWt="182." delays="14" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="255.025" peakThrust="330.314" throatDia="0." exitDia="0."\r
+Itot="382.538" burn-time="1.5" massFrac="19265.8" Isp="0.39" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="100182." cg="129."/>\r
+<eng-data t="0.009" f="253.24" m="99883.6" cg="129."/>\r
+<eng-data t="0.055" f="255.442" m="96819.6" cg="129."/>\r
+<eng-data t="0.219" f="277.463" m="85375.5" cg="129."/>\r
+<eng-data t="0.482" f="301.686" m="65430.7" cg="129."/>\r
+<eng-data t="0.67" f="323.707" m="50035.1" cg="129."/>\r
+<eng-data t="0.735" f="330.314" m="44468.5" cg="129."/>\r
+<eng-data t="0.797" f="323.707" m="39158.8" cg="129."/>\r
+<eng-data t="1.001" f="297.282" m="22570.6" cg="129."/>\r
+<eng-data t="1.162" f="266.453" m="10686." cg="129."/>\r
+<eng-data t="1.205" f="259.847" m="7722.6" cg="129."/>\r
+<eng-data t="1.236" f="237.826" m="5702.42" cg="129."/>\r
+<eng-data t="1.363" f="50.6481" m="905.132" cg="129."/>\r
+<eng-data t="1.428" f="26.4251" m="249.135" cg="129."/>\r
+<eng-data t="1.5" f="0." m="0." cg="129."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; KBA I301W\r
-I301W 38 369.6 18 0.295031 0.724 KBA\r
- 0.0080 266.093\r
- 0.014 327.114\r
- 0.03 354.124\r
- 0.058 350.122\r
- 0.107 335.117\r
- 0.133 326.114\r
- 0.189 326.114\r
- 0.217 333.116\r
- 0.237 383.134\r
- 0.253 402.14\r
- 0.287 395.138\r
- 0.33 381.133\r
- 0.72 381.133\r
- 1.035 341.119\r
- 1.437 317.111\r
- 1.57 262.092\r
- 1.698 130.045\r
- 1.789 83.029\r
- 1.833 74.026\r
- 1.867 53.019\r
- 1.893 23.008\r
- 1.916 13.005\r
- 1.952 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-Aerotech" code="I301W" Type="reloadable" dia="38." len="369.6"\r
+initWt="724." propWt="295.031" delays="18" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="302.243" peakThrust="402.14" throatDia="0." exitDia="0."\r
+Itot="589.979" burn-time="1.95" massFrac="40.75" Isp="203.91" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>KBA I301W</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="295.031" cg="184.8"/>\r
+<eng-data t="0.008" f="266.093" m="294.499" cg="184.8"/>\r
+<eng-data t="0.014" f="327.114" m="293.609" cg="184.8"/>\r
+<eng-data t="0.03" f="354.124" m="290.883" cg="184.8"/>\r
+<eng-data t="0.058" f="350.122" m="285.953" cg="184.8"/>\r
+<eng-data t="0.107" f="335.117" m="277.558" cg="184.8"/>\r
+<eng-data t="0.133" f="326.114" m="273.259" cg="184.8"/>\r
+<eng-data t="0.189" f="326.114" m="264.127" cg="184.8"/>\r
+<eng-data t="0.217" f="333.116" m="259.511" cg="184.8"/>\r
+<eng-data t="0.237" f="383.134" m="255.93" cg="184.8"/>\r
+<eng-data t="0.253" f="402.14" m="252.788" cg="184.8"/>\r
+<eng-data t="0.287" f="395.138" m="246.01" cg="184.8"/>\r
+<eng-data t="0.33" f="381.133" m="237.664" cg="184.8"/>\r
+<eng-data t="0.72" f="381.133" m="163.333" cg="184.8"/>\r
+<eng-data t="1.035" f="341.119" m="106.447" cg="184.8"/>\r
+<eng-data t="1.437" f="317.111" m="40.2858" cg="184.8"/>\r
+<eng-data t="1.57" f="262.092" m="21.0246" cg="184.8"/>\r
+<eng-data t="1.698" f="130.045" m="8.47441" cg="184.8"/>\r
+<eng-data t="1.789" f="83.029" m="3.6263" cg="184.8"/>\r
+<eng-data t="1.833" f="74.026" m="1.89845" cg="184.8"/>\r
+<eng-data t="1.867" f="53.019" m="0.818411" cg="184.8"/>\r
+<eng-data t="1.893" f="23.008" m="0.324166" cg="184.8"/>\r
+<eng-data t="1.916" f="13.005" m="0.117062" cg="184.8"/>\r
+<eng-data t="1.952" f="0." m="0." cg="184.8"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Kosdon by AeroTech I310S\r
-;Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
-;provided by ThrustCurve.org (www.thrustcurve.org)\r
-I310S 38 368 6-0 0.312256 0.713216 Kosdon-by-AeroTech \r
-0.045 334.66\r
-0.136 314.409\r
-0.228 322.556\r
-0.32 326.871\r
-0.411 331.851\r
-0.503 335.911\r
-0.595 336.933\r
-0.686 340.151\r
-0.778 342.066\r
-0.87 344.722\r
-0.961 348.578\r
-1.053 349.548\r
-1.146 351.943\r
-1.239 347.939\r
-1.33 345.079\r
-1.422 337.035\r
-1.514 333.332\r
-1.605 323.832\r
-1.697 289\r
-1.789 215.097\r
-1.88 136.596\r
-1.972 83.863\r
-2.064 37.922\r
-2.155 20.736\r
-2.248 5.943\r
-2.341 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-AeroTech" code="I310S" Type="reloadable" dia="38." len="368."\r
+initWt="713.216" propWt="312.256" delays="6,14,1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="265.458" peakThrust="351.943" throatDia="0."\r
+exitDia="0." Itot="621.438" burn-time="2.34" massFrac="43.78" Isp="202.94"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Kosdon by AeroTech I310S\r
+Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+provided by ThrustCurve.org (www.thrustcurve.org)\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="312.256" cg="184."/>\r
+<eng-data t="0.045" f="334.66" m="308.472" cg="184."/>\r
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+<eng-data t="0.595" f="336.933" m="217.853" cg="184."/>\r
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+<eng-data t="0.778" f="342.066" m="186.605" cg="184."/>\r
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+<eng-data t="0.961" f="348.578" m="154.88" cg="184."/>\r
+<eng-data t="1.053" f="349.548" m="138.744" cg="184."/>\r
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+<eng-data t="1.239" f="347.939" m="106." cg="184."/>\r
+<eng-data t="1.33" f="345.079" m="90.1563" cg="184."/>\r
+<eng-data t="1.422" f="337.035" m="74.39" cg="184."/>\r
+<eng-data t="1.514" f="333.332" m="58.8953" cg="184."/>\r
+<eng-data t="1.605" f="323.832" m="43.8709" cg="184."/>\r
+<eng-data t="1.697" f="289." m="29.706" cg="184."/>\r
+<eng-data t="1.789" f="215.097" m="18.0544" cg="184."/>\r
+<eng-data t="1.88" f="136.596" m="10.0138" cg="184."/>\r
+<eng-data t="1.972" f="83.863" m="4.9182" cg="184."/>\r
+<eng-data t="2.064" f="37.922" m="2.10328" cg="184."/>\r
+<eng-data t="2.155" f="20.736" m="0.762213" cg="184."/>\r
+<eng-data t="2.248" f="5.943" m="0.138858" cg="184."/>\r
+<eng-data t="2.341" f="0." m="0." cg="184."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Kosdon by AeroTech I370F\r
-;Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
-;provided by ThrustCurve.org (www.thrustcurve.org)\r
-I370F 38 368 100 0.312256 0.705152 Kosdon-by-AeroTech \r
-0.035 373.074\r
-0.109 389.927\r
-0.184 401.07\r
-0.259 416.613\r
-0.334 429.598\r
-0.409 438.025\r
-0.484 443.83\r
-0.559 447.326\r
-0.634 446.764\r
-0.709 447.263\r
-0.784 444.735\r
-0.859 441.302\r
-0.933 435.676\r
-1.007 425.29\r
-1.082 414.897\r
-1.157 404.222\r
-1.232 395.358\r
-1.307 382.062\r
-1.382 334.152\r
-1.457 275.974\r
-1.532 179.654\r
-1.607 83.023\r
-1.682 39.608\r
-1.757 16.105\r
-1.832 4.151\r
-1.907 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-AeroTech" code="I370F" Type="reloadable" dia="38." len="368."\r
+initWt="705.152" propWt="312.256" delays="1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="330.108" peakThrust="447.326" throatDia="0."\r
+exitDia="0." Itot="629.515" burn-time="1.91" massFrac="44.28" Isp="205.58"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Kosdon by AeroTech I370F\r
+Copyright Tripoli Motor Testing 2001 (www.tripoli.org)\r
+provided by ThrustCurve.org (www.thrustcurve.org)\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="312.256" cg="184."/>\r
+<eng-data t="0.035" f="373.074" m="309.018" cg="184."/>\r
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+<eng-data t="0.859" f="441.302" m="133.899" cg="184."/>\r
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+<eng-data t="1.457" f="275.974" m="17.1325" cg="184."/>\r
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+<eng-data t="1.607" f="83.023" m="3.77137" cg="184."/>\r
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+<eng-data t="1.832" f="4.151" m="0.0772126" cg="184."/>\r
+<eng-data t="1.907" f="0." m="0." cg="184."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-I450F 38 370 14 0.3032 0.73 Kosdon-by-AeroTech \r
-0.012 634.202\r
-0.037 550.523\r
-0.108 519.693\r
-0.241 510.885\r
-0.639 550.523\r
-0.729 554.927\r
-0.809 546.118\r
-0.939 497.672\r
-1.072 471.247\r
-1.128 440.418\r
-1.165 387.568\r
-1.211 206.996\r
-1.295 88.0836\r
-1.36 26.4251\r
-1.41 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-AeroTech" code="I450F" Type="reloadable" dia="38." len="370."\r
+initWt="730." propWt="303.2" delays="14" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="449.448" peakThrust="634.202" throatDia="0." exitDia="0."\r
+Itot="633.722" burn-time="1.41" massFrac="41.53" Isp="213.13" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="303.2" cg="185."/>\r
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+<eng-data t="1.295" f="88.0836" m="2.09662" cg="185."/>\r
+<eng-data t="1.36" f="26.4251" m="0.316073" cg="185."/>\r
+<eng-data t="1.41" f="0." m="0." cg="185."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J405S 38 476 14 0.367 0.88 Kosdon-by-AeroTech \r
-0.009 528.502\r
-0.024 488.864\r
-0.046 462.439\r
-0.136 462.439\r
-0.268 458.035\r
-0.986 453.631\r
-1.421 444.822\r
-1.523 255.442\r
-1.697 92.4878\r
-1.93 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-AeroTech" code="J405S" Type="reloadable" dia="38." len="476."\r
+initWt="880." propWt="367." delays="14" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="374.25" peakThrust="528.502" throatDia="0." exitDia="0."\r
+Itot="722.303" burn-time="1.93" massFrac="41.7" Isp="200.69" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="367." cg="238."/>\r
+<eng-data t="0.009" f="528.502" m="365.792" cg="238."/>\r
+<eng-data t="0.024" f="488.864" m="361.915" cg="238."/>\r
+<eng-data t="0.046" f="462.439" m="356.598" cg="238."/>\r
+<eng-data t="0.136" f="462.439" m="335.451" cg="238."/>\r
+<eng-data t="0.268" f="458.035" m="304.584" cg="238."/>\r
+<eng-data t="0.986" f="453.631" m="138.29" cg="238."/>\r
+<eng-data t="1.421" f="444.822" m="39.0006" cg="238."/>\r
+<eng-data t="1.523" f="255.442" m="20.8547" cg="238."/>\r
+<eng-data t="1.697" f="92.4878" m="5.47466" cg="238."/>\r
+<eng-data t="1.93" f="0." m="0." cg="238."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-Aerotech" code="J520F" Type="reloadable" dia="38." len="368."\r
+initWt="722." propWt="327." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="514.335" peakThrust="737.092" throatDia="0." exitDia="0."\r
+Itot="645.491" burn-time="1.25" massFrac="45.29" Isp="201.29" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve and engine data TRA certification dated Nov. 25,\r
+2007.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="327." cg="184."/>\r
+<eng-data t="0.018" f="696.864" m="323.823" cg="184."/>\r
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+<eng-data t="1.039" f="552.819" m="26.5292" cg="184."/>\r
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+<eng-data t="1.1" f="330.913" m="12.8726" cg="184."/>\r
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+<eng-data t="1.161" f="224.502" m="4.50913" cg="184."/>\r
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+<eng-data t="1.255" f="0." m="0." cg="184."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-J605F 38 476 14 0.367 0.88 Kosdon-by-AeroTech \r
-0.024 886.341\r
-0.037 704.669\r
-0.077 660.627\r
-0.438 704.669\r
-0.506 715.679\r
-0.59 710.174\r
-0.853 655.122\r
-0.973 594.564\r
-1.041 412.892\r
-1.091 324.808\r
-1.177 132.125\r
-1.3 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-AeroTech" code="J605F" Type="reloadable" dia="38." len="476."\r
+initWt="880." propWt="367." delays="14,1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="567.604" peakThrust="886.341" throatDia="0." exitDia="0."\r
+Itot="737.885" burn-time="1.3" massFrac="41.7" Isp="205.02" tDiv="10" tStep="-1."\r
+tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="367." cg="238."/>\r
+<eng-data t="0.024" f="886.341" m="361.71" cg="238."/>\r
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+<eng-data t="0.853" f="655.122" m="77.3163" cg="238."/>\r
+<eng-data t="0.973" f="594.564" m="40.0231" cg="238."/>\r
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+<eng-data t="1.177" f="132.125" m="4.04146" cg="238."/>\r
+<eng-data t="1.3" f="0." m="0." cg="238."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Kosdon-by-Aerotech" code="J740G" Type="reloadable" dia="38." len="370."\r
+initWt="724." propWt="308." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="788.072" peakThrust="956.51" throatDia="0." exitDia="0."\r
+Itot="665.133" burn-time="0.84" massFrac="42.54" Isp="220.21" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Animal Compatible. Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve and engine data TRA certification dated Oct 14,\r
+2008.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="308." cg="185."/>\r
+<eng-data t="0.003" f="84.03" m="307.942" cg="185."/>\r
+<eng-data t="0.009" f="94.757" m="307.693" cg="185."/>\r
+<eng-data t="0.015" f="459.483" m="306.923" cg="185."/>\r
+<eng-data t="0.026" f="661.512" m="304.068" cg="185."/>\r
+<eng-data t="0.039" f="740.178" m="299.849" cg="185."/>\r
+<eng-data t="0.044" f="763.42" m="298.109" cg="185."/>\r
+<eng-data t="0.054" f="775.935" m="294.545" cg="185."/>\r
+<eng-data t="0.07" f="783.087" m="288.769" cg="185."/>\r
+<eng-data t="0.078" f="792.026" m="285.852" cg="185."/>\r
+<eng-data t="0.087" f="827.784" m="282.476" cg="185."/>\r
+<eng-data t="0.119" f="856.39" m="269.998" cg="185."/>\r
+<eng-data t="0.167" f="884.996" m="250.645" cg="185."/>\r
+<eng-data t="0.241" f="902.874" m="220.013" cg="185."/>\r
+<eng-data t="0.323" f="918.965" m="185.424" cg="185."/>\r
+<eng-data t="0.421" f="918.965" m="143.721" cg="185."/>\r
+<eng-data t="0.464" f="915.389" m="125.458" cg="185."/>\r
+<eng-data t="0.495" f="911.814" m="112.344" cg="185."/>\r
+<eng-data t="0.546" f="908.238" m="90.8521" cg="185."/>\r
+<eng-data t="0.568" f="915.389" m="81.5631" cg="185."/>\r
+<eng-data t="0.589" f="920.753" m="72.6354" cg="185."/>\r
+<eng-data t="0.616" f="938.632" m="61.0117" cg="185."/>\r
+<eng-data t="0.634" f="947.571" m="53.1508" cg="185."/>\r
+<eng-data t="0.649" f="956.51" m="46.5379" cg="185."/>\r
+<eng-data t="0.659" f="949.359" m="42.1252" cg="185."/>\r
+<eng-data t="0.681" f="913.601" m="32.6358" cg="185."/>\r
+<eng-data t="0.7" f="870.693" m="24.7865" cg="185."/>\r
+<eng-data t="0.715" f="831.359" m="18.8753" cg="185."/>\r
+<eng-data t="0.727" f="781.299" m="14.3947" cg="185."/>\r
+<eng-data t="0.736" f="693.693" m="11.3211" cg="185."/>\r
+<eng-data t="0.751" f="548.876" m="7.0057" cg="185."/>\r
+<eng-data t="0.765" f="362.938" m="4.05009" cg="185."/>\r
+<eng-data t="0.772" f="185.938" m="3.16051" cg="185."/>\r
+<eng-data t="0.78" f="286.059" m="2.28625" cg="185."/>\r
+<eng-data t="0.788" f="173.423" m="1.43517" cg="185."/>\r
+<eng-data t="0.793" f="116.212" m="1.09987" cg="185."/>\r
+<eng-data t="0.807" f="59." m="0.531928" cg="185."/>\r
+<eng-data t="0.828" f="28.606" m="0.105972" cg="185."/>\r
+<eng-data t="0.844" f="0." m="0." cg="185."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-K1750R 54.0 728.00 0 1.25300 2.56000 KBA\r
- 0.02 1309.09 \r
- 0.03 1679.77 \r
- 0.05 1736.54 \r
- 0.11 1689.79 \r
- 0.26 1799.99 \r
- 0.40 1913.54 \r
- 0.46 1896.84 \r
- 0.68 2023.74 \r
- 0.90 2133.94 \r
- 0.95 2097.21 \r
- 1.00 2050.46 \r
- 1.05 1920.21 \r
- 1.10 1793.31 \r
- 1.16 1676.43 \r
- 1.21 1719.85 \r
- 1.25 1526.15 \r
- 1.27 1302.41 \r
- 1.32 874.95 \r
- 1.35 454.17 \r
- 1.36 317.25 \r
- 1.37 200.37 \r
- 1.40 90.17 \r
- 1.46 0.00 \r
-;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="KOS" code="K1750R" Type="reloadable" dia="54." len="727." initWt="2564."\r
+propWt="1441." auto-calc-mass="1" auto-calc-cg="1" avgThrust="1690.93"\r
+peakThrust="2133.94" throatDia="0." exitDia="0." Itot="2468.76" burn-time="1.46"\r
+massFrac="56.2" Isp="174.7" tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1."\r
+FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>MFR data converted from RASP file from Mark Koelsch</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="1441." cg="363.5"/>\r
+ <eng-data t="0.02" f="1309.09" m="1433.36" cg="363.5"/>\r
+ <eng-data t="0.03" f="1679.77" m="1424.64" cg="363.5"/>\r
+ <eng-data t="0.05" f="1679.77" m="1405.03" cg="363.5"/>\r
+ <eng-data t="0.11" f="1736.54" m="1345.2" cg="363.5"/>\r
+ <eng-data t="0.26" f="1689.79" m="1195.21" cg="363.5"/>\r
+ <eng-data t="0.4" f="1799.99" m="1052.62" cg="363.5"/>\r
+ <eng-data t="0.46" f="1913.54" m="987.596" cg="363.5"/>\r
+ <eng-data t="0.68" f="1896.84" m="742.945" cg="363.5"/>\r
+ <eng-data t="0.9" f="2023.74" m="491.22" cg="363.5"/>\r
+ <eng-data t="0.95" f="2133.94" m="430.549" cg="363.5"/>\r
+ <eng-data t="1." f="2097.21" m="368.807" cg="363.5"/>\r
+ <eng-data t="1.05" f="2050.46" m="308.283" cg="363.5"/>\r
+ <eng-data t="1.1" f="1920.21" m="250.342" cg="363.5"/>\r
+ <eng-data t="1.16" f="1793.31" m="185.315" cg="363.5"/>\r
+ <eng-data t="1.21" f="1676.43" m="134.683" cg="363.5"/>\r
+ <eng-data t="1.25" f="1719.85" m="95.0355" cg="363.5"/>\r
+ <eng-data t="1.27" f="1526.15" m="76.0889" cg="363.5"/>\r
+ <eng-data t="1.32" f="1302.41" m="34.8136" cg="363.5"/>\r
+ <eng-data t="1.35" f="874.95" m="15.7499" cg="363.5"/>\r
+ <eng-data t="1.36" f="454.17" m="11.8709" cg="363.5"/>\r
+ <eng-data t="1.37" f="317.25" m="9.61956" cg="363.5"/>\r
+ <eng-data t="1.4" f="200.37" m="5.08759" cg="363.5"/>\r
+ <eng-data t="1.46" f="90.17" m="0." cg="363.5"/>\r
+ <eng-data t="1.46" f="90.17" m="0." cg="363.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-K400S 54 403 6-10-14 0.713216 1.50931 Kosdon-by-AeroTech \r
-0.074 465.928\r
-0.225 441.922\r
-0.377 442.414\r
-0.529 445.492\r
-0.681 449.048\r
-0.833 451.88\r
-0.985 454.481\r
-1.138 456.929\r
-1.29 458.237\r
-1.442 457.021\r
-1.594 455.62\r
-1.746 451.772\r
-1.897 446.421\r
-2.048 438.843\r
-2.2 429.377\r
-2.352 419.003\r
-2.504 408.274\r
-2.656 397.608\r
-2.808 388.018\r
-2.96 367.07\r
-3.113 263.666\r
-3.265 114.378\r
-3.417 46.238\r
-3.569 8.62\r
-3.721 2.401\r
-3.873 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-AeroTech" code="K400S" Type="reloadable" dia="54." len="403."\r
+initWt="1509.31" propWt="713.216" delays="6,10,14" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="354.68" peakThrust="465.928" throatDia="0."\r
+exitDia="0." Itot="1373.67" burn-time="3.87" massFrac="47.25" Isp="196.4"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="713.216" cg="201.5"/>\r
+<eng-data t="0.074" f="465.928" m="704.265" cg="201.5"/>\r
+<eng-data t="0.225" f="441.922" m="668.678" cg="201.5"/>\r
+<eng-data t="0.377" f="442.414" m="633.782" cg="201.5"/>\r
+<eng-data t="0.529" f="445.492" m="598.746" cg="201.5"/>\r
+<eng-data t="0.681" f="449.048" m="563.448" cg="201.5"/>\r
+<eng-data t="0.833" f="451.88" m="527.898" cg="201.5"/>\r
+<eng-data t="0.985" f="454.481" m="492.133" cg="201.5"/>\r
+<eng-data t="1.138" f="456.929" m="455.933" cg="201.5"/>\r
+<eng-data t="1.29" f="458.237" m="419.821" cg="201.5"/>\r
+<eng-data t="1.442" f="457.021" m="383.706" cg="201.5"/>\r
+<eng-data t="1.594" f="455.62" m="347.693" cg="201.5"/>\r
+<eng-data t="1.746" f="451.772" m="311.888" cg="201.5"/>\r
+<eng-data t="1.897" f="446.421" m="276.679" cg="201.5"/>\r
+<eng-data t="2.048" f="438.843" m="241.977" cg="201.5"/>\r
+<eng-data t="2.2" f="429.377" m="207.718" cg="201.5"/>\r
+<eng-data t="2.352" f="419.003" m="174.241" cg="201.5"/>\r
+<eng-data t="2.504" f="408.274" m="141.597" cg="201.5"/>\r
+<eng-data t="2.656" f="397.608" m="109.797" cg="201.5"/>\r
+<eng-data t="2.808" f="388.018" m="78.7971" cg="201.5"/>\r
+<eng-data t="2.96" f="367.07" m="49.0017" cg="201.5"/>\r
+<eng-data t="3.113" f="263.666" m="23.9495" cg="201.5"/>\r
+<eng-data t="3.265" f="114.378" m="9.0321" cg="201.5"/>\r
+<eng-data t="3.417" f="46.238" m="2.69429" cg="201.5"/>\r
+<eng-data t="3.569" f="8.62" m="0.529624" cg="201.5"/>\r
+<eng-data t="3.721" f="2.401" m="0.0947421" cg="201.5"/>\r
+<eng-data t="3.873" f="0." m="0." cg="201.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-Aerotech" code="K700F" Type="reloadable" dia="54." len="406."\r
+initWt="1503." propWt="734." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="776.225" peakThrust="912.317" throatDia="0." exitDia="0."\r
+Itot="1436.02" burn-time="1.85" massFrac="48.84" Isp="199.5" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve and engine data TRA certification dated Nov 25,\r
+2007.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="734." cg="203."/>\r
+<eng-data t="0.011" f="789.955" m="731.779" cg="203."/>\r
+<eng-data t="0.029" f="815.147" m="724.395" cg="203."/>\r
+<eng-data t="0.045" f="831.342" m="717.663" cg="203."/>\r
+<eng-data t="0.057" f="753.966" m="712.801" cg="203."/>\r
+<eng-data t="0.084" f="746.768" m="702.445" cg="203."/>\r
+<eng-data t="0.118" f="741.37" m="689.514" cg="203."/>\r
+<eng-data t="0.184" f="757.565" m="664.231" cg="203."/>\r
+<eng-data t="0.422" f="800.752" m="569.446" cg="203."/>\r
+<eng-data t="0.454" f="818.746" m="556.202" cg="203."/>\r
+<eng-data t="0.748" f="872.729" m="429.109" cg="203."/>\r
+<eng-data t="0.798" f="870.93" m="406.828" cg="203."/>\r
+<eng-data t="0.853" f="890.724" m="382.066" cg="203."/>\r
+<eng-data t="0.923" f="903.32" m="349.971" cg="203."/>\r
+<eng-data t="1." f="912.317" m="314.241" cg="203."/>\r
+<eng-data t="1.084" f="908.718" m="275.148" cg="203."/>\r
+<eng-data t="1.209" f="897.921" m="217.433" cg="203."/>\r
+<eng-data t="1.315" f="872.729" m="169.466" cg="203."/>\r
+<eng-data t="1.395" f="843.938" m="134.368" cg="203."/>\r
+<eng-data t="1.454" f="815.147" m="109.351" cg="203."/>\r
+<eng-data t="1.517" f="786.356" m="83.5657" cg="203."/>\r
+<eng-data t="1.565" f="777.359" m="64.3832" cg="203."/>\r
+<eng-data t="1.587" f="775.559" m="55.6519" cg="203."/>\r
+<eng-data t="1.61" f="786.356" m="46.4709" cg="203."/>\r
+<eng-data t="1.635" f="753.966" m="36.6294" cg="203."/>\r
+<eng-data t="1.658" f="656.796" m="28.3369" cg="203."/>\r
+<eng-data t="1.678" f="543.431" m="22.2021" cg="203."/>\r
+<eng-data t="1.694" f="494.846" m="17.9565" cg="203."/>\r
+<eng-data t="1.71" f="446.262" m="14.1082" cg="203."/>\r
+<eng-data t="1.753" f="300.507" m="5.90163" cg="203."/>\r
+<eng-data t="1.773" f="208.735" m="3.29871" cg="203."/>\r
+<eng-data t="1.796" f="131.359" m="1.29961" cg="203."/>\r
+<eng-data t="1.814" f="50.384" m="0.463556" cg="203."/>\r
+<eng-data t="1.85" f="0." m="0." cg="203."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Kosdon by Aerotech K750 White Lightning.\r
-K750W 54 728 0 1.315 2.62 KBA\r
- 0.0080 266.075\r
- 0.012 457.102\r
- 0.02 750.467\r
- 0.032 999.485\r
- 0.044 1112.055\r
- 0.06 1180.279\r
- 0.095 1098.41\r
- 0.127 1057.476\r
- 0.163 1040.42\r
- 0.334 1050.653\r
- 0.62 1054.064\r
- 0.998 975.607\r
- 1.324 907.382\r
- 1.69 903.971\r
- 2.06 886.915\r
- 2.184 828.924\r
- 2.299 757.289\r
- 2.394 651.541\r
- 2.502 556.028\r
- 2.609 450.28\r
- 2.784 327.476\r
- 2.999 245.607\r
- 3.039 201.261\r
- 3.134 92.103\r
- 3.206 40.935\r
- 3.337 6.822\r
- 3.468 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-Aerotech" code="K750W" Type="reloadable" dia="54." len="728."\r
+initWt="2620." propWt="1315." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="731.984" peakThrust="1180.28" throatDia="0." exitDia="0."\r
+Itot="2538.52" burn-time="3.47" massFrac="50.19" Isp="196.85" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Kosdon by Aerotech K750 White Lightning.</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="1315." cg="364."/>\r
+<eng-data t="0.008" f="266.075" m="1314.45" cg="364."/>\r
+<eng-data t="0.012" f="457.102" m="1313.7" cg="364."/>\r
+<eng-data t="0.02" f="750.467" m="1311.2" cg="364."/>\r
+<eng-data t="0.032" f="999.485" m="1305.76" cg="364."/>\r
+<eng-data t="0.044" f="1112.06" m="1299.2" cg="364."/>\r
+<eng-data t="0.06" f="1180.28" m="1289.7" cg="364."/>\r
+<eng-data t="0.095" f="1098.41" m="1269.04" cg="364."/>\r
+<eng-data t="0.127" f="1057.48" m="1251.17" cg="364."/>\r
+<eng-data t="0.163" f="1040.42" m="1231.61" cg="364."/>\r
+<eng-data t="0.334" f="1050.65" m="1138.99" cg="364."/>\r
+<eng-data t="0.62" f="1054.06" m="983.083" cg="364."/>\r
+<eng-data t="0.998" f="975.607" m="784.368" cg="364."/>\r
+<eng-data t="1.324" f="907.382" m="625.374" cg="364."/>\r
+<eng-data t="1.69" f="903.971" m="453.662" cg="364."/>\r
+<eng-data t="2.06" f="886.915" m="282.036" cg="364."/>\r
+<eng-data t="2.184" f="828.924" m="226.928" cg="364."/>\r
+<eng-data t="2.299" f="757.289" m="179.681" cg="364."/>\r
+<eng-data t="2.394" f="651.541" m="145.015" cg="364."/>\r
+<eng-data t="2.502" f="556.028" m="111.236" cg="364."/>\r
+<eng-data t="2.609" f="450.28" m="83.3473" cg="364."/>\r
+<eng-data t="2.784" f="327.476" m="48.0943" cg="364."/>\r
+<eng-data t="2.999" f="245.607" m="16.181" cg="364."/>\r
+<eng-data t="3.039" f="201.261" m="11.5513" cg="364."/>\r
+<eng-data t="3.134" f="92.103" m="4.33286" cg="364."/>\r
+<eng-data t="3.206" f="40.935" m="1.85188" cg="364."/>\r
+<eng-data t="3.337" f="6.822" m="0.231472" cg="364."/>\r
+<eng-data t="3.468" f="0." m="0." cg="364."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Kosdon by AeroTech L1000S\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-L1000S 54 728 0 1.232 2.32512 KBA\r
- 0.055 795.305\r
- 0.175 981.574\r
- 0.295 989.173\r
- 0.415 1008.634\r
- 0.535 1028.836\r
- 0.655 1048.483\r
- 0.775 1067.573\r
- 0.895 1087.034\r
- 1.015 1108.719\r
- 1.135 1131.516\r
- 1.255 1156.908\r
- 1.375 1177.296\r
- 1.498 1199.596\r
- 1.620 1212.881\r
- 1.740 1227.153\r
- 1.860 1232.342\r
- 1.980 1249.950\r
- 2.100 1026.056\r
- 2.220 737.107\r
- 2.340 565.851\r
- 2.460 313.414\r
- 2.580 89.706\r
- 2.700 20.758\r
- 2.820 8.526\r
- 2.942 5.338\r
- 3.065 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-AeroTech" code="L1000S" Type="reloadable" dia="54." len="727.96"\r
+initWt="2325" propWt="1301." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="960.255" peakThrust="1310.24" throatDia="0." exitDia="0."\r
+Itot="2592.69" burn-time="2.7" massFrac="104.25" Isp="203.21" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="1301." cg="363.98"/>\r
+<eng-data t="0.038" f="1310.24" m="1288.51" cg="363.98"/>\r
+<eng-data t="0.085" f="1090.03" m="1260.2" cg="363.98"/>\r
+<eng-data t="0.139" f="1023.97" m="1231.56" cg="363.98"/>\r
+<eng-data t="0.216" f="1001.95" m="1192.42" cg="363.98"/>\r
+<eng-data t="0.479" f="979.93" m="1061.65" cg="363.98"/>\r
+<eng-data t="1.035" f="1112.06" m="769.815" cg="363.98"/>\r
+<eng-data t="1.993" f="1244.18" m="203.469" cg="363.98"/>\r
+<eng-data t="2.047" f="1222.16" m="170.054" cg="363.98"/>\r
+<eng-data t="2.094" f="1189.13" m="141.619" cg="363.98"/>\r
+<eng-data t="2.179" f="924.878" m="96.5355" cg="363.98"/>\r
+<eng-data t="2.233" f="737.7" m="74.0101" cg="363.98"/>\r
+<eng-data t="2.264" f="847.805" m="61.6783" cg="363.98"/>\r
+<eng-data t="2.295" f="682.648" m="49.7747" cg="363.98"/>\r
+<eng-data t="2.295" f="539.512" m="49.7747" cg="363.98"/>\r
+<eng-data t="2.302" f="649.617" m="47.6862" cg="363.98"/>\r
+<eng-data t="2.318" f="451.428" m="43.2662" cg="363.98"/>\r
+<eng-data t="2.7" f="0." m="0." cg="363.98"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-L1400F 54 727 100 1.248 2.502 Kosdon-by-AeroTech \r
-0.037 1541.46\r
-0.061 1453.38\r
-0.166 1354.29\r
-1.001 1772.68\r
-1.279 1783.69\r
-1.329 1882.79\r
-1.387 1992.89\r
-1.486 1387.32\r
-1.604 869.826\r
-1.65 748.711\r
-1.666 726.69\r
-1.69 924.878\r
-1.697 594.564\r
-1.758 319.303\r
-1.88 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-AeroTech" code="L1400F" Type="reloadable" dia="54." len="727."\r
+initWt="2502." propWt="1248." delays="14,1000" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="1403.07" peakThrust="1992.89" throatDia="0."\r
+exitDia="0." Itot="2637.77" burn-time="1.88" massFrac="49.88" Isp="215.53"\r
+tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
+mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<data>\r
+<eng-data t="0." f="0." m="1248." cg="363.5"/>\r
+<eng-data t="0.037" f="1541.46" m="1234.51" cg="363.5"/>\r
+<eng-data t="0.061" f="1453.38" m="1217.5" cg="363.5"/>\r
+<eng-data t="0.166" f="1354.29" m="1147.76" cg="363.5"/>\r
+<eng-data t="1.001" f="1772.68" m="530.092" cg="363.5"/>\r
+<eng-data t="1.279" f="1783.69" m="296.209" cg="363.5"/>\r
+<eng-data t="1.329" f="1882.79" m="252.841" cg="363.5"/>\r
+<eng-data t="1.387" f="1992.89" m="199.664" cg="363.5"/>\r
+<eng-data t="1.486" f="1387.32" m="120.5" cg="363.5"/>\r
+<eng-data t="1.604" f="869.826" m="57.4929" cg="363.5"/>\r
+<eng-data t="1.65" f="748.711" m="39.8801" cg="363.5"/>\r
+<eng-data t="1.666" f="726.69" m="34.2957" cg="363.5"/>\r
+<eng-data t="1.69" f="924.878" m="24.9189" cg="363.5"/>\r
+<eng-data t="1.697" f="594.564" m="22.4028" cg="363.5"/>\r
+<eng-data t="1.758" f="319.303" m="9.21533" cg="363.5"/>\r
+<eng-data t="1.88" f="0." m="0." cg="363.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-Aerotech" code="L2300G" Type="reloadable" dia="54." len="728."\r
+initWt="2630." propWt="1310." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="2191.39" peakThrust="2930.02" throatDia="0." exitDia="0."\r
+Itot="2737.05" burn-time="1.25" massFrac="49.81" Isp="213.05" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Animal Compatible. Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve and engine data TRA certification dated Oct 14,\r
+2008.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="1310." cg="364."/>\r
+<eng-data t="0.013" f="2930.02" m="1300.88" cg="364."/>\r
+<eng-data t="0.019" f="2243.45" m="1293.46" cg="364."/>\r
+<eng-data t="0.029" f="2277.3" m="1282.64" cg="364."/>\r
+<eng-data t="0.033" f="2499.71" m="1278.07" cg="364."/>\r
+<eng-data t="0.043" f="2480.37" m="1266.15" cg="364."/>\r
+<eng-data t="0.054" f="2533.55" m="1252.95" cg="364."/>\r
+<eng-data t="0.07" f="2504.54" m="1233.66" cg="364."/>\r
+<eng-data t="0.088" f="2470.7" m="1212.23" cg="364."/>\r
+<eng-data t="0.11" f="2451.36" m="1186.31" cg="364."/>\r
+<eng-data t="0.151" f="2446.52" m="1138.26" cg="364."/>\r
+<eng-data t="0.207" f="2480.37" m="1072.23" cg="364."/>\r
+<eng-data t="0.277" f="2533.55" m="988.239" cg="364."/>\r
+<eng-data t="0.443" f="2654.43" m="782.145" cg="364."/>\r
+<eng-data t="0.503" f="2717.28" m="705.015" cg="364."/>\r
+<eng-data t="0.528" f="2741.46" m="672.357" cg="364."/>\r
+<eng-data t="0.575" f="2794.64" m="610.089" cg="364."/>\r
+<eng-data t="0.603" f="2823.65" m="572.443" cg="364."/>\r
+<eng-data t="0.636" f="2842.99" m="527.692" cg="364."/>\r
+<eng-data t="0.651" f="2915.52" m="507.021" cg="364."/>\r
+<eng-data t="0.664" f="2891.34" m="488.956" cg="364."/>\r
+<eng-data t="0.686" f="2872." m="458.613" cg="364."/>\r
+<eng-data t="0.729" f="2857.5" m="399.655" cg="364."/>\r
+<eng-data t="0.757" f="2833.32" m="361.523" cg="364."/>\r
+<eng-data t="0.772" f="2794.64" m="341.32" cg="364."/>\r
+<eng-data t="0.794" f="2780.14" m="311.97" cg="364."/>\r
+<eng-data t="0.804" f="2852.66" m="298.49" cg="364."/>\r
+<eng-data t="0.812" f="2789.81" m="287.688" cg="364."/>\r
+<eng-data t="0.83" f="2722.12" m="263.945" cg="364."/>\r
+<eng-data t="0.855" f="2630.25" m="231.923" cg="364."/>\r
+<eng-data t="0.874" f="2577.07" m="208.246" cg="364."/>\r
+<eng-data t="0.912" f="2509.38" m="161.991" cg="364."/>\r
+<eng-data t="0.93" f="2519.05" m="140.331" cg="364."/>\r
+<eng-data t="0.943" f="2461.03" m="124.838" cg="364."/>\r
+<eng-data t="0.977" f="2354.66" m="85.6552" cg="364."/>\r
+<eng-data t="0.991" f="2224.11" m="70.3148" cg="364."/>\r
+<eng-data t="0.997" f="2354.66" m="63.7404" cg="364."/>\r
+<eng-data t="1.013" f="1885.66" m="47.5044" cg="364."/>\r
+<eng-data t="1.042" f="1426.33" m="24.5193" cg="364."/>\r
+<eng-data t="1.061" f="937.994" m="13.7691" cg="364."/>\r
+<eng-data t="1.074" f="498.007" m="9.30163" cg="364."/>\r
+<eng-data t="1.096" f="246.586" m="5.3815" cg="364."/>\r
+<eng-data t="1.117" f="149.886" m="3.38903" cg="364."/>\r
+<eng-data t="1.136" f="106.37" m="2.22387" cg="364."/>\r
+<eng-data t="1.172" f="48.35" m="0.890936" cg="364."/>\r
+<eng-data t="1.249" f="0." m="0." cg="364."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; KBA M1450W\r
-M1450W 75 1038.9 0 4.15 7.6000000000000005 KBA\r
- 0.035 1842.929\r
- 0.076 2287.088\r
- 0.146 1968.884\r
- 0.215 1882.704\r
- 0.291 1836.299\r
- 0.499 1862.816\r
- 1.005 1935.738\r
- 1.559 1889.333\r
- 2.155 1816.412\r
- 2.862 1750.119\r
- 3.493 1663.939\r
- 3.853 1358.994\r
- 4.221 1060.678\r
- 4.484 788.88\r
- 4.761 523.71\r
- 4.942 258.54\r
- 5.323 258.54\r
- 5.6 172.36\r
- 5.801 119.326\r
- 5.96 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-Aerotech" code="M1450W" Type="reloadable" dia="75." len="1038.9"\r
+initWt="7600." propWt="4150." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="1353.98" peakThrust="2287.09" throatDia="0." exitDia="0."\r
+Itot="8069.72" burn-time="5.96" massFrac="54.61" Isp="198.28" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>KBA M1450W</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="4150." cg="519.45"/>\r
+<eng-data t="0.035" f="1842.93" m="4133.41" cg="519.45"/>\r
+<eng-data t="0.076" f="2287.09" m="4089.87" cg="519.45"/>\r
+<eng-data t="0.146" f="1968.88" m="4013.27" cg="519.45"/>\r
+<eng-data t="0.215" f="1882.7" m="3944.93" cg="519.45"/>\r
+<eng-data t="0.291" f="1836.3" m="3872.26" cg="519.45"/>\r
+<eng-data t="0.499" f="1862.82" m="3674.41" cg="519.45"/>\r
+<eng-data t="1.005" f="1935.74" m="3180.18" cg="519.45"/>\r
+<eng-data t="1.559" f="1889.33" m="2635.29" cg="519.45"/>\r
+<eng-data t="2.155" f="1816.41" m="2067.38" cg="519.45"/>\r
+<eng-data t="2.862" f="1750.12" m="1419.01" cg="519.45"/>\r
+<eng-data t="3.493" f="1663.94" m="865.069" cg="519.45"/>\r
+<eng-data t="3.853" f="1358.99" m="585.242" cg="519.45"/>\r
+<eng-data t="4.221" f="1060.68" m="356.279" cg="519.45"/>\r
+<eng-data t="4.484" f="788.88" m="231.2" cg="519.45"/>\r
+<eng-data t="4.761" f="523.71" m="137.71" cg="519.45"/>\r
+<eng-data t="4.942" f="258.54" m="101.303" cg="519.45"/>\r
+<eng-data t="5.323" f="258.54" m="50.6454" cg="519.45"/>\r
+<eng-data t="5.6" f="172.36" m="19.9541" cg="519.45"/>\r
+<eng-data t="5.801" f="119.326" m="4.87856" cg="519.45"/>\r
+<eng-data t="5.96" f="0." m="0." cg="519.45"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-Aerotech" code="M2900R" Type="reloadable" dia="75." len="1039."\r
+initWt="7195." propWt="3755." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="2264.18" peakThrust="3102.43" throatDia="0." exitDia="0."\r
+Itot="5460.99" burn-time="2.41" massFrac="52.19" Isp="148.3" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>@File: 070616w11.txt, @Pts-I: 1207, @Pts-O: 32, @Sm: 5, @CO: 5%\r
+@TI: 5460.0, @TIa: 5447.69, @TIe: 0.0%, @ThMax: 3102.43, @ThAvg: 2675.68, @Tb: 2.036\r
+Exported using ThrustCurveTool, www.ThrustGear.com\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="3755." cg="519.5"/>\r
+<eng-data t="0." f="2.43719" m="3755." cg="519.5"/>\r
+<eng-data t="0.034" f="19.468" m="3754.74" cg="519.5"/>\r
+<eng-data t="0.05" f="69.6872" m="3754.25" cg="519.5"/>\r
+<eng-data t="0.052" f="166.128" m="3754.09" cg="519.5"/>\r
+<eng-data t="0.056" f="533.998" m="3753.13" cg="519.5"/>\r
+<eng-data t="0.06" f="1067.23" m="3750.93" cg="519.5"/>\r
+<eng-data t="0.064" f="1683.24" m="3747.14" cg="519.5"/>\r
+<eng-data t="0.066" f="1897.53" m="3744.68" cg="519.5"/>\r
+<eng-data t="0.072" f="2294.77" m="3736.03" cg="519.5"/>\r
+<eng-data t="0.082" f="2495.75" m="3719.56" cg="519.5"/>\r
+<eng-data t="0.102" f="2708.42" m="3683.78" cg="519.5"/>\r
+<eng-data t="0.108" f="2734.74" m="3672.55" cg="519.5"/>\r
+<eng-data t="0.204" f="2696.52" m="3493.29" cg="519.5"/>\r
+<eng-data t="0.438" f="2690.17" m="3059.94" cg="519.5"/>\r
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+<eng-data t="1.8639" f="2744.09" m="205.022" cg="519.5"/>\r
+<eng-data t="1.8979" f="2565.3" m="142.959" cg="519.5"/>\r
+<eng-data t="1.9079" f="2455.92" m="125.696" cg="519.5"/>\r
+<eng-data t="1.9599" f="1357.39" m="57.5225" cg="519.5"/>\r
+<eng-data t="1.9879" f="857.187" m="36.2039" cg="519.5"/>\r
+<eng-data t="2.0059" f="603.283" m="27.1659" cg="519.5"/>\r
+<eng-data t="2.0259" f="417.576" m="20.1464" cg="519.5"/>\r
+<eng-data t="2.0439" f="303.914" m="15.6815" cg="519.5"/>\r
+<eng-data t="2.0899" f="150.616" m="8.49318" cg="519.5"/>\r
+<eng-data t="2.1419" f="73.2216" m="4.49148" cg="519.5"/>\r
+<eng-data t="2.2259" f="25.6056" m="1.63741" cg="519.5"/>\r
+<eng-data t="2.4119" f="0." m="0." cg="519.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+; @File: M3500.txt, @Pts-I: 1176, @Pts-O: 32, @Sm: 3, @CO: 5%\r
+; @TI: 7311.23, @TIa: 7305.44, @TIe: 0.0%, @ThMax: 4059.41, @ThAvg: 3454.11, @Tb: 2.115\r
+; Exported using ThrustCurveTool, www.ThrustGear.com\r
+M3500 75 1039 0 3.755 7.173 AT/RCS\r
+0.0 0.371006\r
+0.106 8.86696\r
+0.122 135.5975\r
+0.13 670.948\r
+0.14 1587.827\r
+0.156 2299.92\r
+0.178 2751.17\r
+0.188 2731.01\r
+0.196 2914.16\r
+0.2 2842.83\r
+0.208 2985.3\r
+0.21 2903.6\r
+0.248 3027.96\r
+0.932 3723.01\r
+1.5879 4059.41\r
+1.9859 3900.58\r
+2.0279 3759.75\r
+2.0399 3495.75\r
+2.0539 3522.63\r
+2.0739 3313.47\r
+2.0819 2962.24\r
+2.0899 2964.52\r
+2.1039 2484.66\r
+2.1639 1015.768\r
+2.1879 602.438\r
+2.1979 218.762\r
+2.2059 440.947\r
+2.2119 274.648\r
+2.2199 474.133\r
+2.2219 353.742\r
+2.2399 180.0836\r
+2.3499 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="Kosdon-by-Aerotech" code="M3500R" Type="reloadable" dia="75." len="1039."\r
+initWt="7173." propWt="3755." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="3111.64" peakThrust="4059.41" throatDia="0." exitDia="0."\r
+Itot="7312.05" burn-time="2.35" massFrac="52.35" Isp="198.57" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>@File: M3500.txt, @Pts-I: 1176, @Pts-O: 32, @Sm: 3, @CO: 5%\r
+@TI: 7311.23, @TIa: 7305.44, @TIe: 0.0%, @ThMax: 4059.41, @ThAvg: 3454.11, @Tb: 2.115\r
+Exported using ThrustCurveTool, www.ThrustGear.com\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="3755." cg="519.5"/>\r
+<eng-data t="0." f="0.371006" m="3755." cg="519.5"/>\r
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+<eng-data t="0.178" f="2751.17" m="3702.19" cg="519.5"/>\r
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+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+ <data>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+ <eng-data t="1.5" f="0." m="0." cg="63.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+H100-SP 38 178 5-8-10-13-17 0.12 0.335 Loki \r
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+++ /dev/null
-;\r
-;\r
-H144 38 178 5-8-10-13-17 0.12 0.335 Loki \r
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-1.4 44.6\r
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-1.6 0\r
--- /dev/null
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+ <engine-list>\r
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+ </data>\r
+ </engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+ <data>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
-;\r
-;\r
-H500 38 292 5-7-9-12-15 0.16 0.454 Loki \r
+H500-LW 38 292 5-7-9-12-15 0.16 0.454 Loki \r
0.001 189.286\r
0.0116009 534.733\r
0.099768 539.465\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+ <data>\r
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+ </data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+ <data>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+I110-LW 38 292 5-8-12 0.289 0.589 Loki \r
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--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Loki" code="I210-LR" Type="reloadable" dia="38." len="292." initWt="540."\r
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+ <data>\r
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+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+I316-SP 38 292 5-8-10-13-17 0.24 0.54 Loki \r
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+++ /dev/null
-;\r
-;\r
-I405 38 292 5-8-10-13-17 0.24 0.54 Loki \r
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--- /dev/null
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+ <engine-list>\r
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+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+;\r
+;\r
+I430-LB 38 292 7-9-12-15 0.24 0.54 Loki \r
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--- /dev/null
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+ <engine-list>\r
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+ <eng-data t="1.25" f="0." m="0." cg="312.5"/>\r
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+ </engine>\r
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--- /dev/null
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--- /dev/null
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--- /dev/null
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--- /dev/null
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--- /dev/null
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+++ /dev/null
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--- /dev/null
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+++ /dev/null
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--- /dev/null
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--- /dev/null
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--- /dev/null
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--- /dev/null
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--- /dev/null
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+++ /dev/null
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--- /dev/null
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+++ /dev/null
-;\r
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--- /dev/null
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--- /dev/null
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--- /dev/null
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+++ /dev/null
-;\r
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--- /dev/null
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+++ /dev/null
-;\r
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--- /dev/null
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--- /dev/null
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--- /dev/null
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+ </data>\r
+ </engine>\r
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--- /dev/null
+<engine-database>\r
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+ </data>\r
+ </engine>\r
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--- /dev/null
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+++ /dev/null
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--- /dev/null
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+ </engine-list>\r
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--- /dev/null
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+++ /dev/null
-;\r
-;\r
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--- /dev/null
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+ </engine-list>\r
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--- /dev/null
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--- /dev/null
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+ </engine>\r
+</engine-list>\r
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--- /dev/null
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+ <eng-data t="0.5" f="3856.81" m="3296.79" cg="519."/>\r
+ <eng-data t="1.25" f="3983.83" m="1849.78" cg="519."/>\r
+ <eng-data t="2." f="2644.34" m="626.54" cg="519."/>\r
+ <eng-data t="2.5" f="1224.02" m="150.597" cg="519."/>\r
+ <eng-data t="3." f="0." m="0." cg="519."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Loki" code="M900-LR" Type="reloadable" dia="75." len="785." initWt="5530."\r
+propWt="3130." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="912.815" peakThrust="1060.69" throatDia="0." exitDia="0."\r
+Itot="5476.89" burn-time="6." massFrac="56.6" Isp="178.43" tDiv="10" tStep="-1."\r
+tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="3130." cg="392.5"/>\r
+ <eng-data t="0.02" f="807.388" m="3125.39" cg="392.5"/>\r
+ <eng-data t="1." f="992.084" m="2621.48" cg="392.5"/>\r
+ <eng-data t="2." f="1050.13" m="2037.92" cg="392.5"/>\r
+ <eng-data t="3." f="1060.69" m="1434.76" cg="392.5"/>\r
+ <eng-data t="4." f="992.084" m="848.191" cg="392.5"/>\r
+ <eng-data t="5." f="923.483" m="300.825" cg="392.5"/>\r
+ <eng-data t="5.5" f="591.029" m="84.4422" cg="392.5"/>\r
+ <eng-data t="6." f="0." m="0." cg="392.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="Loki" code="N3800-LW" Type="reloadable" dia="98." len="1016."\r
+initWt="11600." propWt="6125." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="3851.56" peakThrust="4965.36" throatDia="0." exitDia="0."\r
+Itot="12517.6" burn-time="3.25" massFrac="52.8" Isp="208.4" tDiv="10" tStep="-1."\r
+tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+ <data>\r
+ <eng-data t="0." f="0." m="6125." cg="508."/>\r
+ <eng-data t="0.01" f="4780.6" m="6113.3" cg="508."/>\r
+ <eng-data t="0.5" f="4572.75" m="4992.01" cg="508."/>\r
+ <eng-data t="1." f="4688.22" m="3859.13" cg="508."/>\r
+ <eng-data t="1.5" f="4965.36" m="2678.23" cg="508."/>\r
+ <eng-data t="2." f="3972.29" m="1584.9" cg="508."/>\r
+ <eng-data t="2.5" f="3002.31" m="731.709" cg="508."/>\r
+ <eng-data t="3." f="1986.14" m="121.48" cg="508."/>\r
+ <eng-data t="3.25" f="0." m="0." cg="508."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-F50T 29.0 98.00 4-6-9 0.03790 0.08490 AT\r
- 0.01 37.97 \r
- 0.02 56.27 \r
- 0.03 65.08 \r
- 0.12 71.86 \r
- 0.23 75.25 \r
- 0.33 77.29 \r
- 0.35 77.70 \r
- 0.45 75.25 \r
- 0.59 71.86 \r
- 0.72 65.76 \r
- 0.83 58.98 \r
- 1.01 43.39 \r
- 1.19 25.76 \r
- 1.25 15.59 \r
- 1.30 8.81 \r
- 1.36 4.75 \r
- 1.42 0.00 \r
-;\r
+++ /dev/null
-;\r
-;\r
-A6Q 18 70 4 0.0035 0.0153 Quest \r
-0.1 4.8\r
-0.2 11.82\r
-0.23 7.9\r
-0.3 4.8\r
-0.41 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="60.46" Itot="2.075" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="5.062" burn-time="0.41" cgDiv="10" cgFix="1" cgStep="-1." code="A6Q" delays="4" dia="18." exitDia="0." initWt="15.3" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="22.88" mfg="Quest" peakThrust="11.82" propWt="3.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+ <eng-data cg="35." f="0." m="3.5" t="0."/>\r
+ <eng-data cg="35." f="4.8" m="3.09524" t="0.1"/>\r
+ <eng-data cg="35." f="11.82" m="1.69376" t="0.2"/>\r
+ <eng-data cg="35." f="7.9" m="1.19489" t="0.23"/>\r
+ <eng-data cg="35." f="4.8" m="0.445237" t="0.3"/>\r
+ <eng-data cg="35." f="0." m="-0." t="0.41"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+;Quest A8 RASP.ENG file made from NAR published data\r
+; File produced Aug 2009\r
+; The total impulse, peak thrust, average thrust and burn time are\r
+; the same as the averaged static test data on the NAR web site in\r
+; the certification file. The curve drawn with these data points is as\r
+; close to the certification curve as can be with such a limited\r
+; number of points (32) allowed with wRASP up to v1.6.\r
+A8 18 69 3- 0.0063 0.0131 QU\r
+0.073 2.139\r
+0.085 2.599\r
+0.097 3.317\r
+0.110 4.035\r
+0.122 4.34\r
+0.135 4.955\r
+0.147 5.569\r
+0.160 6.132\r
+0.173 6.85\r
+0.185 7.361\r
+0.197 7.976\r
+0.210 8.281\r
+0.222 8.741\r
+0.235 9.407\r
+0.247 9.712\r
+0.260 11.14\r
+0.273 10.063\r
+0.285 8.768\r
+0.297 6.647\r
+0.310 5.042\r
+0.322 3.953\r
+0.335 3.019\r
+0.347 2.136\r
+0.360 1.512\r
+0.372 1.043\r
+0.380 0.000\r
--- /dev/null
+;QUEST B4 RASP.ENG file made from NAR published data\r
+; File produced SEPTEMBER, 2009\r
+; The total impulse, peak thrust, average thrust and burn time are\r
+; the same as the averaged static test data on the NAR web site in\r
+; the certification file. The curve drawn with these data points is as\r
+; close to the certification curve as can be with such a limited\r
+; number of points (32) allowed with wRASP up to v1.6.\r
+B4 19 70 4- 0.0104 0.0166 Q\r
+0.033 1.091\r
+0.061 2.250\r
+0.104 4.228\r
+0.138 6.002\r
+0.184 8.457\r
+0.222 10.504\r
+0.258 12.810\r
+0.275 9.412\r
+0.289 6.070\r
+0.298 4.842\r
+0.309 4.228\r
+0.329 3.751\r
+0.359 3.546\r
+0.444 3.410\r
+0.550 3.274\r
+0.646 3.478\r
+0.723 3.615\r
+0.787 3.751\r
+0.814 3.751\r
+0.831 3.478\r
+0.843 2.796\r
+0.862 1.773\r
+0.882 0.818\r
+0.904 0.136\r
+0.910 0.0\r
+++ /dev/null
-;\r
-;\r
-B6Q 18 70 0-2-4 0.0065 0.0162 Quest \r
-0.1 7\r
-0.18 14.38\r
-0.2 10.2\r
-0.24 6.6\r
-0.3 6\r
-0.4 6.1\r
-0.5 6.2\r
-0.6 6.3\r
-0.65 6.6\r
-0.7 3\r
-0.75 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="72.91" Itot="4.647" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="6.197" burn-time="0.75" cgDiv="10" cgFix="1" cgStep="-1." code="B6Q" delays="4" dia="18." exitDia="0." initWt="16.2" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="40.12" mfg="Quest" peakThrust="14.38" propWt="6.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="35." f="0." m="6.5" t="0."/>\r
+<eng-data cg="35." f="7." m="6.01049" t="0.1"/>\r
+<eng-data cg="35." f="14.38" m="4.81441" t="0.18"/>\r
+<eng-data cg="35." f="10.2" m="4.47063" t="0.2"/>\r
+<eng-data cg="35." f="6.6" m="4.0007" t="0.24"/>\r
+<eng-data cg="35." f="6." m="3.47203" t="0.3"/>\r
+<eng-data cg="35." f="6.1" m="2.62587" t="0.4"/>\r
+<eng-data cg="35." f="6.2" m="1.76573" t="0.5"/>\r
+<eng-data cg="35." f="6.3" m="0.891608" t="0.6"/>\r
+<eng-data cg="35." f="6.6" m="0.440559" t="0.65"/>\r
+<eng-data cg="35." f="3." m="0.104895" t="0.7"/>\r
+<eng-data cg="35." f="0." m="-0." t="0.75"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Quest C6-0 from NAR data\r
-C6-0 18 70 0 0.0083 0.0216 Q\r
- 0.02 0.497\r
- 0.057 2.539\r
- 0.089 5.132\r
- 0.129 7.947\r
- 0.159 9.437\r
- 0.171 21.247\r
- 0.181 23.234\r
- 0.194 22.958\r
- 0.204 22.185\r
- 0.218 19.592\r
- 0.233 17.881\r
- 0.258 10.486\r
- 0.308 2.428\r
- 0.338 2.539\r
- 0.385 2.98\r
- 0.412 3.091\r
- 0.442 3.422\r
- 0.459 2.98\r
- 0.536 3.256\r
- 0.732 3.311\r
- 0.747 2.483\r
- 0.78 2.98\r
- 1.323 3.587\r
- 1.365 2.815\r
- 1.887 3.808\r
- 1.974 3.256\r
- 2.1 3.532\r
- 2.227 3.201\r
- 2.247 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="79.14" Itot="8.537" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="5.238" burn-time="1.63" cgDiv="10" cgFix="1" cgStep="-1." code="C6" delays="0,3,5" dia="18." exitDia="0." initWt="20.4" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="53.92" mfg="Quest" peakThrust="13.4" propWt="11." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="35." f="0." m="11." t="0."/>\r
+<eng-data cg="35." f="3.8" m="10.8776" t="0.05"/>\r
+<eng-data cg="35." f="6.5" m="10.5458" t="0.1"/>\r
+<eng-data cg="35." f="11.75" m="9.95798" t="0.15"/>\r
+<eng-data cg="35." f="13.4" m="9.14788" t="0.2"/>\r
+<eng-data cg="35." f="9.25" m="8.4183" t="0.25"/>\r
+<eng-data cg="35." f="7." m="7.89488" t="0.3"/>\r
+<eng-data cg="35." f="5.6" m="7.08316" t="0.4"/>\r
+<eng-data cg="35." f="5.2" m="6.38741" t="0.5"/>\r
+<eng-data cg="35." f="5.05" m="5.72709" t="0.6"/>\r
+<eng-data cg="35." f="4.8" m="5.09253" t="0.7"/>\r
+<eng-data cg="35." f="4.5" m="4.49341" t="0.8"/>\r
+<eng-data cg="35." f="4.6" m="3.90717" t="0.9"/>\r
+<eng-data cg="35." f="4.45" m="3.32416" t="1."/>\r
+<eng-data cg="35." f="4.2" m="2.20966" t="1.2"/>\r
+<eng-data cg="35." f="4." m="1.41728" t="1.35"/>\r
+<eng-data cg="35." f="4." m="0.0257687" t="1.62"/>\r
+<eng-data cg="35." f="0." m="-0." t="1.63"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; Quest D5-0 by Mark Koelsch from NAR data\r
-D5-0 20 88 0 0.025 0.0384 Q\r
- 0.096 1.241\r
- 0.252 5.897\r
- 0.304 8.586\r
- 0.357 10.552\r
- 0.391 11.483\r
- 0.435 9.828\r
- 0.557 6.103\r
- 0.583 5.172\r
- 0.67 5.172\r
- 1.078 4.966\r
- 1.2 4.345\r
- 1.73 4.759\r
- 1.8 4.759\r
- 1.887 4.138\r
- 2.391 5.069\r
- 2.626 4.966\r
- 3.009 5.379\r
- 3.357 5.276\r
- 3.661 5.69\r
- 3.835 3.103\r
- 3.887 1.655\r
- 3.983 0.0\r
--- /dev/null
+; QUEST D5 RASP.ENG FILE\r
+; The total impulse, peak thrust, average thrust and burn time are\r
+; the same as the averaged static test data on the NAR web site in\r
+; the certification file. The curve drawn with these data points is as\r
+; close to the certification curve as can be with such a limited\r
+; number of points (32) allowed with wRASP up to v1.6.\r
+D5 20 96 4-6 0.0240 0.451 QUEST\r
+0.010 1.014\r
+0.122 2.652\r
+0.172 4.836\r
+0.273 7.723\r
+0.331 10.610\r
+0.390 13.809\r
+0.448 16.800\r
+0.480 12.403\r
+0.484 8.266\r
+0.517 5.221\r
+0.713 4.125\r
+0.974 4.121\r
+1.135 3.338\r
+1.324 3.101\r
+1.550 3.254\r
+1.971 3.169\r
+2.393 3.162\r
+2.752 3.391\r
+3.069 3.386\r
+3.547 3.301\r
+3.694 3.064\r
+3.948 3.294\r
+4.215 3.290\r
+4.412 3.287\r
+4.496 2.505\r
+4.586 1.801\r
+4.610 0.000\r
+;\r
--- /dev/null
+; QUEST D8 RASP.ENG FILE\r
+; The total impulse, peak thrust, average thrust and burn time are\r
+; the same as the averaged static test data on the NAR web site in\r
+; the certification file. The curve drawn with these data points is as\r
+; close to the certification curve as can be with such a limited\r
+; number of points (32) allowed with wRASP up to v1.6.\r
+D8 24 70 0-3-5 0.0220 0.454 QUEST\r
+0.002 1.014\r
+0.010 1.565\r
+0.130 5.178\r
+0.217 8.911\r
+0.298 14.812\r
+0.351 20.231\r
+0.414 25.289\r
+0.442 28.882\r
+0.470 23.844\r
+0.487 17.461\r
+0.508 13.367\r
+0.537 10.958\r
+0.600 9.152\r
+0.673 8.791\r
+0.828 8.309\r
+0.933 8.068\r
+1.136 7.105\r
+1.350 6.743\r
+1.480 6.623\r
+1.602 6.502\r
+1.648 7.105\r
+1.683 6.382\r
+1.743 6.262\r
+1.865 6.141\r
+1.974 6.141\r
+2.104 6.262\r
+2.132 5.419\r
+2.170 3.492\r
+2.191 1.926\r
+2.200 0.000\r
+;\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="77.28" Itot="0.303" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="0.37" burn-time="0.82" cgDiv="10" cgFix="1" cgStep="-1." code="Micro Maxx" delays="1" dia="6." exitDia="0." initWt="1.07" len="16." mDiv="10" mFix="1" mStep="-1." massFrac="37.38" mfg="Quest" peakThrust="1.24" propWt="0.4" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <data>\r
+ <eng-data cg="8." f="0." m="0.4" t="0."/>\r
+ <eng-data cg="8." f="0.24" m="0.398416" t="0.01"/>\r
+ <eng-data cg="8." f="1.24" m="0.349592" t="0.06"/>\r
+ <eng-data cg="8." f="0.394366" m="0.30193" t="0.104199"/>\r
+ <eng-data cg="8." f="0.267606" m="0.0125636" t="0.766719"/>\r
+ <eng-data cg="8." f="0.14" m="0.000923713" t="0.81"/>\r
+ <eng-data cg="8." f="0." m="-0." t="0.82"/>\r
+ </data>\r
+ </engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="60.9" Itot="0.299" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="0.452" burn-time="0.66" cgDiv="10" cgFix="1" cgStep="-1." code="Micro Maxx II" delays="1" dia="6." exitDia="0." initWt="1.2" len="26." mDiv="10" mFix="1" mStep="-1." massFrac="41.67" mfg="Quest" peakThrust="3.21" propWt="0.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <comments>QUEST MICROMAXX II RASP.ENG file made from NAR published data\r
+File produced Dec 29, 2001\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+ <data>\r
+ <eng-data cg="13." f="0." m="0.5" t="0."/>\r
+ <eng-data cg="13." f="0.16" m="0.498928" t="0.008"/>\r
+ <eng-data cg="13." f="0.482" m="0.493554" t="0.018"/>\r
+ <eng-data cg="13." f="0.993" m="0.486144" t="0.024"/>\r
+ <eng-data cg="13." f="1.534" m="0.473451" t="0.03"/>\r
+ <eng-data cg="13." f="2.032" m="0.461509" t="0.034"/>\r
+ <eng-data cg="13." f="2.397" m="0.454093" t="0.036"/>\r
+ <eng-data cg="13." f="2.543" m="0.43755" t="0.04"/>\r
+ <eng-data cg="13." f="3.025" m="0.40958" t="0.046"/>\r
+ <eng-data cg="13." f="3.21" m="0.37826" t="0.052"/>\r
+ <eng-data cg="13." f="2.864" m="0.342664" t="0.059"/>\r
+ <eng-data cg="13." f="2.191" m="0.300344" t="0.069"/>\r
+ <eng-data cg="13." f="1.094" m="0.270091" t="0.08"/>\r
+ <eng-data cg="13." f="0.539" m="0.260521" t="0.087"/>\r
+ <eng-data cg="13." f="0.378" m="0.256683" t="0.092"/>\r
+ <eng-data cg="13." f="0.304" m="0.248689" t="0.106"/>\r
+ <eng-data cg="13." f="0.26" m="0.233107" t="0.139"/>\r
+ <eng-data cg="13." f="0.303" m="0.215196" t="0.177"/>\r
+ <eng-data cg="13." f="0.287" m="0.192474" t="0.223"/>\r
+ <eng-data cg="13." f="0.243" m="0.176944" t="0.258"/>\r
+ <eng-data cg="13." f="0.198" m="0.165868" t="0.288"/>\r
+ <eng-data cg="13." f="0.27" m="0.143143" t="0.346"/>\r
+ <eng-data cg="13." f="0.298" m="0.116513" t="0.402"/>\r
+ <eng-data cg="13." f="0.254" m="0.112354" t="0.411"/>\r
+ <eng-data cg="13." f="0.312" m="0.10335" t="0.43"/>\r
+ <eng-data cg="13." f="0.282" m="0.0859449" t="0.465"/>\r
+ <eng-data cg="13." f="0.238" m="0.0694017" t="0.503"/>\r
+ <eng-data cg="13." f="0.281" m="0.0637531" t="0.516"/>\r
+ <eng-data cg="13." f="0.28" m="0.0421482" t="0.562"/>\r
+ <eng-data cg="13." f="0.294" m="0.0137954" t="0.621"/>\r
+ <eng-data cg="13." f="0.279" m="0.00420109" t="0.641"/>\r
+ <eng-data cg="13." f="0.176" m="0.00191552" t="0.647"/>\r
+ <eng-data cg="13." f="0." m="-0." t="0.66"/>\r
+ </data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
; RATT Works H70H\r
-; Copyright Tripoli Motor Testing 2002 (www.tripoli.org)\r
+; converted from TMT test stand data 2002 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
H70H 29 457 0 0.106176 0.348992 RTW\r
0.051 124.137\r
; RATT Works I80H\r
-; Copyright Tripoli Motor Testing 2002 (www.tripoli.org)\r
+; converted from TMT test stand data 2002 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
I80H 29 730 0 0.21952 0.549248 RTW\r
0.093 84.101\r
; RATT Works I90LH\r
-; Copyright Tripoli Motor Testing 2002 (www.tripoli.org)\r
+; converted from TMT test stand data 2002 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
I90LH 29 921 0 0.285376 0.684544 RTW\r
0.127 137.737\r
; RATT Works K240H\r
-; Copyright Tripoli Motor Testing 2002 (www.tripoli.org)\r
+; converted from TMT test stand data 2002 (www.tripoli.org)\r
; provided by ThrustCurve.org (www.thrustcurve.org)\r
K240H 64 908 0 1.29338 2.81434 RTW\r
0.164 413.978\r
--- /dev/null
+; RocketVision E15 RASP.ENG file made from NAR published data\r
+; File produced December 10, 2000\r
+; The total impulse, peak thrust, average thrust and burn time are\r
+; the same as the averaged static test data on the NAR web site in\r
+; the certification file. The curve drawn with these data points is as\r
+; close to the certification curve as can be with such a limited\r
+; number of points (32) allowed with wRASP up to v1.6.\r
+E15 24 70 4-7 .0201 .0501 RV\r
+0.020 23.330\r
+0.036 27.318\r
+0.058 28.840\r
+0.079 27.171\r
+0.139 25.638\r
+0.183 24.263\r
+0.237 24.106\r
+0.297 22.426\r
+0.373 21.964\r
+0.400 20.894\r
+0.443 21.355\r
+0.487 20.442\r
+0.617 19.833\r
+0.742 18.457\r
+0.812 20.000\r
+0.850 18.006\r
+0.899 18.467\r
+1.035 17.711\r
+1.100 16.945\r
+1.160 16.945\r
+1.377 15.736\r
+1.426 14.656\r
+1.436 16.198\r
+1.463 14.813\r
+1.550 14.361\r
+1.572 15.432\r
+1.610 13.752\r
+1.827 12.839\r
+2.126 10.098\r
+2.337 6.116\r
+2.538 1.369\r
+2.640 0.000\r
+++ /dev/null
-;ROADRUNNER E25R WRASP FILE\r
-E25R 29 76 4-7 0.02 0.078 RR\r
- 0.0 1.15995\r
- 0.0 4.0904\r
- 0.01 13.9194\r
- 0.02 24.481\r
- 0.025 28.327\r
- 0.04 33.028\r
- 0.045 33.639\r
- 0.07 33.516\r
- 0.12 35.287\r
- 0.195 36.569\r
- 0.245 38.278\r
- 0.28 37.668\r
- 0.315 38.657\r
- 0.35 37.729\r
- 0.385 37.973\r
- 0.45 36.691\r
- 0.56 36.569\r
- 0.73 32.295\r
- 0.82 29.487\r
- 0.9 26.068\r
- 0.92 25.824\r
- 0.945 24.176\r
- 0.995 22.772\r
- 1.035 20.024\r
- 1.08 18.5592\r
- 1.165 14.2247\r
- 1.19 13.6142\r
- 1.31 7.2039\r
- 1.395 4.2735\r
- 1.445 3.602\r
- 1.49 2.1978\r
- 1.505 0.79365\r
- 1.506 0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="RR" code="E25R" Type="single-use" dia="29." len="76." initWt="78."\r
+propWt="20." delays="4,7" auto-calc-mass="1" auto-calc-cg="1" avgThrust="25.68"\r
+peakThrust="38.657" throatDia="0." exitDia="0." Itot="38.674" burn-time="1.51"\r
+massFrac="25.64" Isp="197.18" tDiv="10" tStep="-1." tFix="1" FDiv="10"\r
+FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."\r
+cgFix="1">\r
+ <comments>ROADRUNNER E25R WRASP FILE</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="20." cg="38."/>\r
+ <eng-data t="0." f="1.15995" m="20." cg="38."/>\r
+ <eng-data t="0." f="4.0904" m="20." cg="38."/>\r
+ <eng-data t="0.01" f="13.9194" m="19.9534" cg="38."/>\r
+ <eng-data t="0.02" f="24.481" m="19.8541" cg="38."/>\r
+ <eng-data t="0.025" f="28.327" m="19.7859" cg="38."/>\r
+ <eng-data t="0.04" f="33.028" m="19.5479" cg="38."/>\r
+ <eng-data t="0.045" f="33.639" m="19.4617" cg="38."/>\r
+ <eng-data t="0.07" f="33.516" m="19.0276" cg="38."/>\r
+ <eng-data t="0.12" f="35.287" m="18.1381" cg="38."/>\r
+ <eng-data t="0.195" f="36.569" m="16.7446" cg="38."/>\r
+ <eng-data t="0.245" f="38.278" m="15.7769" cg="38."/>\r
+ <eng-data t="0.28" f="37.668" m="15.0896" cg="38."/>\r
+ <eng-data t="0.315" f="38.657" m="14.3989" cg="38."/>\r
+ <eng-data t="0.35" f="37.729" m="13.7076" cg="38."/>\r
+ <eng-data t="0.385" f="37.973" m="13.0225" cg="38."/>\r
+ <eng-data t="0.45" f="36.691" m="11.7676" cg="38."/>\r
+ <eng-data t="0.56" f="36.569" m="9.68391" cg="38."/>\r
+ <eng-data t="0.73" f="32.295" m="6.65686" cg="38."/>\r
+ <eng-data t="0.82" f="29.487" m="5.21911" cg="38."/>\r
+ <eng-data t="0.9" f="26.068" m="4.06992" cg="38."/>\r
+ <eng-data t="0.92" f="25.824" m="3.80157" cg="38."/>\r
+ <eng-data t="0.945" f="24.176" m="3.47835" cg="38."/>\r
+ <eng-data t="0.995" f="22.772" m="2.87139" cg="38."/>\r
+ <eng-data t="1.035" f="20.024" m="2.42876" cg="38."/>\r
+ <eng-data t="1.08" f="18.5592" m="1.97982" cg="38."/>\r
+ <eng-data t="1.165" f="14.2247" m="1.25928" cg="38."/>\r
+ <eng-data t="1.19" f="13.6142" m="1.07932" cg="38."/>\r
+ <eng-data t="1.31" f="7.2039" m="0.433366" cg="38."/>\r
+ <eng-data t="1.395" f="4.2735" m="0.181111" cg="38."/>\r
+ <eng-data t="1.445" f="3.602" m="0.0792922" cg="38."/>\r
+ <eng-data t="1.49" f="2.1978" m="0.0118077" cg="38."/>\r
+ <eng-data t="1.505" f="0.79365" m="0.000205214" cg="38."/>\r
+ <eng-data t="1.506" f="0." m="0." cg="38."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-; ROADRUNNER F35 RASP.ENG FILE\r
-; File produced April 5, 2006\r
-; The total impulse, peak thrust, average thrust and burn time are\r
-; the same as the averaged static test data on the NAR web site in\r
-; the certification file. The curve drawn with these data points is as\r
-; close to the certification curve as can be with such a limited\r
-; number of points (32) allowed with wRASP up to v1.6.\r
-F35 29 112 6-10 0.040 0.111 RR\r
-0.023 33.700\r
-0.040 44.462\r
-0.081 47.206\r
-0.121 48.579\r
-0.166 49.270\r
-0.242 49.550\r
-0.315 51.010\r
-0.411 50.111\r
-0.528 49.710\r
-0.664 48.208\r
-0.791 47.256\r
-0.896 46.986\r
-1.000 45.484\r
-1.097 44.943\r
-1.194 42.338\r
-1.277 40.400\r
-1.323 40.706\r
-1.356 37.691\r
-1.402 35.637\r
-1.451 32.753\r
-1.505 29.467\r
-1.578 25.491\r
-1.675 20.833\r
-1.750 17.137\r
-1.828 13.021\r
-1.907 8.638\r
-1.984 5.075\r
-2.049 2.610\r
-2.130 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="194.99" Itot="76.489" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="35.91" burn-time="2.13" cgDiv="10" cgFix="1" cgStep="-1." code="F35" delays="6,10" dia="29." exitDia="0." initWt="111." len="112." mDiv="10" mFix="1" mStep="-1." massFrac="36.04" mfg="Roadrunner Rocketry" peakThrust="51.01" propWt="40." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <comments>ROADRUNNER F35 RASP.ENG FILE\r
+File produced April 5, 2006\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+ <data>\r
+ <eng-data cg="56." f="0." m="40." t="0."/>\r
+ <eng-data cg="56." f="33.7" m="39.7973" t="0.023"/>\r
+ <eng-data cg="56." f="44.462" m="39.4499" t="0.04"/>\r
+ <eng-data cg="56." f="47.206" m="38.4672" t="0.081"/>\r
+ <eng-data cg="56." f="48.579" m="37.4654" t="0.121"/>\r
+ <eng-data cg="56." f="49.27" m="36.314" t="0.166"/>\r
+ <eng-data cg="56." f="49.55" m="34.3503" t="0.242"/>\r
+ <eng-data cg="56." f="51.01" m="32.4308" t="0.315"/>\r
+ <eng-data cg="56." f="50.111" m="29.8925" t="0.411"/>\r
+ <eng-data cg="56." f="49.71" m="26.8387" t="0.528"/>\r
+ <eng-data cg="56." f="48.208" m="23.3567" t="0.664"/>\r
+ <eng-data cg="56." f="47.256" m="20.1866" t="0.791"/>\r
+ <eng-data cg="56." f="46.986" m="17.5992" t="0.896"/>\r
+ <eng-data cg="56." f="45.484" m="15.0846" t="1."/>\r
+ <eng-data cg="56." f="44.943" m="12.7911" t="1.097"/>\r
+ <eng-data cg="56." f="42.338" m="10.5774" t="1.194"/>\r
+ <eng-data cg="56." f="40.4" m="8.78175" t="1.277"/>\r
+ <eng-data cg="56." f="40.706" m="7.80622" t="1.323"/>\r
+ <eng-data cg="56." f="37.691" m="7.12976" t="1.356"/>\r
+ <eng-data cg="56." f="35.637" m="6.24778" t="1.402"/>\r
+ <eng-data cg="56." f="32.753" m="5.37154" t="1.451"/>\r
+ <eng-data cg="56." f="29.467" m="4.49302" t="1.505"/>\r
+ <eng-data cg="56." f="25.491" m="3.444" t="1.578"/>\r
+ <eng-data cg="56." f="20.833" m="2.26908" t="1.675"/>\r
+ <eng-data cg="56." f="17.137" m="1.52446" t="1.75"/>\r
+ <eng-data cg="56." f="13.021" m="0.909384" t="1.828"/>\r
+ <eng-data cg="56." f="8.638" m="0.461984" t="1.907"/>\r
+ <eng-data cg="56." f="5.075" m="0.185892" t="1.984"/>\r
+ <eng-data cg="56." f="2.61" m="0.0552785" t="2.049"/>\r
+ <eng-data cg="56." f="0." m="0." t="2.13"/>\r
+ </data>\r
+ </engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-; ROADRUNNER F45R RASP ENG FILE\r
-F45R 29 93 5-8-14 0.03 0.093 RR\r
- 0.0 4.1971\r
- 0.019 45.500\r
- 0.038 53.070\r
- 0.057 52.402\r
- 0.095 54.741\r
- 0.113 55.298\r
- 0.132 56.744\r
- 0.151 57.190\r
- 0.227 60.419\r
- 0.284 61.754\r
- 0.416 62.422\r
- 0.491 60.753\r
- 0.510 61.420\r
- 0.567 60.307\r
- 0.624 58.414\r
- 0.662 58.080\r
- 0.737 55.298\r
- 0.775 52.959\r
- 0.813 51.513\r
- 0.888 46.169\r
- 0.983 34.701\r
- 1.002 31.807\r
- 1.096 23.902\r
- 1.134 21.453\r
- 1.210 14.106\r
- 1.229 12.992\r
- 1.285 8.4282\r
- 1.342 5.5328\r
- 1.361 5.4218\r
- 1.418 2.9723\r
- 1.420 0.0\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="RR" code="F45R" Type="single-use" dia="29." len="93." initWt="93."\r
+propWt="30." delays="5,8,1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="43.266" peakThrust="62.422" throatDia="0." exitDia="0." Itot="61.438"\r
+burn-time="1.42" massFrac="32.26" Isp="208.83" tDiv="10" tStep="-1." tFix="1"\r
+FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+ <comments>ROADRUNNER F45R RASP ENG FILE</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="30." cg="46.5"/>\r
+ <eng-data t="0." f="4.1971" m="30." cg="46.5"/>\r
+ <eng-data t="0.019" f="45.5" m="29.7695" cg="46.5"/>\r
+ <eng-data t="0.038" f="53.07" m="29.3122" cg="46.5"/>\r
+ <eng-data t="0.057" f="52.402" m="28.823" cg="46.5"/>\r
+ <eng-data t="0.095" f="54.741" m="27.8289" cg="46.5"/>\r
+ <eng-data t="0.113" f="55.298" m="27.3453" cg="46.5"/>\r
+ <eng-data t="0.132" f="56.744" m="26.8256" cg="46.5"/>\r
+ <eng-data t="0.151" f="57.19" m="26.2971" cg="46.5"/>\r
+ <eng-data t="0.227" f="60.419" m="24.1148" cg="46.5"/>\r
+ <eng-data t="0.284" f="61.754" m="22.4146" cg="46.5"/>\r
+ <eng-data t="0.416" f="62.422" m="18.4127" cg="46.5"/>\r
+ <eng-data t="0.491" f="60.753" m="16.1573" cg="46.5"/>\r
+ <eng-data t="0.51" f="61.42" m="15.5905" cg="46.5"/>\r
+ <eng-data t="0.567" f="60.307" m="13.8965" cg="46.5"/>\r
+ <eng-data t="0.624" f="58.414" m="12.2444" cg="46.5"/>\r
+ <eng-data t="0.662" f="58.08" m="11.1636" cg="46.5"/>\r
+ <eng-data t="0.737" f="55.298" m="9.08752" cg="46.5"/>\r
+ <eng-data t="0.775" f="52.959" m="8.08316" cg="46.5"/>\r
+ <eng-data t="0.813" f="51.513" m="7.11391" cg="46.5"/>\r
+ <eng-data t="0.888" f="46.169" m="5.32525" cg="46.5"/>\r
+ <eng-data t="0.983" f="34.701" m="3.44955" cg="46.5"/>\r
+ <eng-data t="1.002" f="31.807" m="3.14104" cg="46.5"/>\r
+ <eng-data t="1.096" f="23.902" m="1.86252" cg="46.5"/>\r
+ <eng-data t="1.134" f="21.453" m="1.44174" cg="46.5"/>\r
+ <eng-data t="1.21" f="14.106" m="0.781934" cg="46.5"/>\r
+ <eng-data t="1.229" f="12.992" m="0.656232" cg="46.5"/>\r
+ <eng-data t="1.285" f="8.4282" m="0.36337" cg="46.5"/>\r
+ <eng-data t="1.342" f="5.5328" m="0.169083" cg="46.5"/>\r
+ <eng-data t="1.361" f="5.4218" m="0.118267" cg="46.5"/>\r
+ <eng-data t="1.418" f="2.9723" m="0.00145136" cg="46.5"/>\r
+ <eng-data t="1.42" f="0." m="0." cg="46.5"/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; ROADRUNNER F60 RASP.ENG FILE\r
-; The total impulse, peak thrust, average thrust and burn time are\r
-; the same as the averaged static test data on the NAR web site in\r
-; the certification file. The curve drawn with these data points is as\r
-; close to the certification curve as can be with such a limited\r
-; number of points (32) allowed with wRASP up to v1.6.\r
-F60R 29 112 4-7-10 0.038 0.109 RR\r
-0.013 45.860\r
-0.021 63.937\r
-0.029 72.291\r
-0.041 75.214\r
-0.061 74.374\r
-0.087 76.872\r
-0.155 83.122\r
-0.231 86.440\r
-0.309 88.088\r
-0.329 90.070\r
-0.345 88.33\r
-0.395 87.90\r
-0.454 87.208\r
-0.514 87.188\r
-0.616 82.141\r
-0.699 77.105\r
-0.765 70.400\r
-0.807 61.611\r
-0.859 51.983\r
-0.926 42.355\r
-0.978 33.556\r
-1.022 21.430\r
-1.061 13.056\r
-1.101 6.776\r
-1.133 3.423\r
-1.190 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="203.52" Itot="75.843" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="63.733" burn-time="1.19" cgDiv="10" cgFix="1" cgStep="-1." code="F60R" delays="4,7,10" dia="29." exitDia="0." initWt="109." len="112." mDiv="10" mFix="1" mStep="-1." massFrac="34.86" mfg="Roadrunner Rocketry" peakThrust="90.07" propWt="38." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <comments>ROADRUNNER F60 RASP.ENG FILE\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+ <data>\r
+ <eng-data cg="56." f="0." m="38." t="0."/>\r
+ <eng-data cg="56." f="45.86" m="37.8506" t="0.013"/>\r
+ <eng-data cg="56." f="63.937" m="37.6306" t="0.021"/>\r
+ <eng-data cg="56." f="72.291" m="37.3576" t="0.029"/>\r
+ <eng-data cg="56." f="75.214" m="36.9141" t="0.041"/>\r
+ <eng-data cg="56." f="74.374" m="36.1646" t="0.061"/>\r
+ <eng-data cg="56." f="76.872" m="35.1795" t="0.087"/>\r
+ <eng-data cg="56." f="83.122" m="32.454" t="0.155"/>\r
+ <eng-data cg="56." f="86.44" m="29.2256" t="0.231"/>\r
+ <eng-data cg="56." f="88.088" m="25.8152" t="0.309"/>\r
+ <eng-data cg="56." f="90.07" m="24.9226" t="0.329"/>\r
+ <eng-data cg="56." f="88.33" m="24.2075" t="0.345"/>\r
+ <eng-data cg="56." f="87.9" m="22.0001" t="0.395"/>\r
+ <eng-data cg="56." f="87.208" m="19.4119" t="0.454"/>\r
+ <eng-data cg="56." f="87.188" m="16.7905" t="0.514"/>\r
+ <eng-data cg="56." f="82.141" m="12.4636" t="0.616"/>\r
+ <eng-data cg="56." f="77.105" m="9.15241" t="0.699"/>\r
+ <eng-data cg="56." f="70.4" m="6.71353" t="0.765"/>\r
+ <eng-data cg="56." f="61.611" m="5.32453" t="0.807"/>\r
+ <eng-data cg="56." f="51.983" m="3.84475" t="0.859"/>\r
+ <eng-data cg="56." f="42.355" m="2.2613" t="0.926"/>\r
+ <eng-data cg="56." f="33.556" m="1.27241" t="0.978"/>\r
+ <eng-data cg="56." f="21.43" m="0.666309" t="1.022"/>\r
+ <eng-data cg="56." f="13.056" m="0.329372" t="1.061"/>\r
+ <eng-data cg="56." f="6.776" m="0.13064" t="1.101"/>\r
+ <eng-data cg="56." f="3.423" m="0.048879" t="1.133"/>\r
+ <eng-data cg="56." f="0." m="0." t="1.19"/>\r
+ </data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-; ROADRUNNER G80 RASP.ENG FILE\r
-; The total impulse, peak thrust, average thrust and burn time are\r
-; the same as the averaged static test data on the NAR web site in\r
-; the certification file. The curve drawn with these data points is as\r
-; close to the certification curve as can be with such a limited\r
-; number of points (32) allowed with wRASP up to v1.6.\r
-G80R 29 140 4-7-10 0.055 0.133 RR\r
-0.012 63.563\r
-0.028 84.077\r
-0.057 89.563\r
-0.119 96.03\r
-0.206 102.518\r
-0.242 104.42\r
-0.297 106.923\r
-0.356 109.826\r
-0.422 111.829\r
-0.483 111.328\r
-0.558 112.632\r
-0.622 112.750\r
-0.683 112.129\r
-0.739 109.125\r
-0.796 102.017\r
-0.863 90.494\r
-0.901 82.750\r
-0.935 72.41\r
-0.976 59.869\r
-1.018 49.826\r
-1.028 44.321\r
-1.042 39.805\r
-1.073 28.272\r
-1.113 18.231\r
-1.170 11.176\r
-1.218 4.636\r
-1.310 0.000\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="194.81" Itot="105.074" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="80.209" burn-time="1.31" cgDiv="10" cgFix="1" cgStep="-1." code="G80R" delays="4,7,10" dia="29." exitDia="0." initWt="133." len="140." mDiv="10" mFix="1" mStep="-1." massFrac="41.35" mfg="Roadrunner Rocketry" peakThrust="112.75" propWt="55." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>ROADRUNNER G80 RASP.ENG FILE\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+ <eng-data cg="70." f="0." m="55." t="0."/>\r
+ <eng-data cg="70." f="63.563" m="54.8004" t="0.012"/>\r
+ <eng-data cg="70." f="84.077" m="54.1821" t="0.028"/>\r
+ <eng-data cg="70." f="89.563" m="52.8642" t="0.057"/>\r
+ <eng-data cg="70." f="96.03" m="49.8527" t="0.119"/>\r
+ <eng-data cg="70." f="102.518" m="45.3318" t="0.206"/>\r
+ <eng-data cg="70." f="104.42" m="43.382" t="0.242"/>\r
+ <eng-data cg="70." f="106.923" m="40.3398" t="0.297"/>\r
+ <eng-data cg="70." f="109.826" m="36.9929" t="0.356"/>\r
+ <eng-data cg="70." f="111.829" m="33.1641" t="0.422"/>\r
+ <eng-data cg="70." f="111.328" m="29.6015" t="0.483"/>\r
+ <eng-data cg="70." f="112.632" m="25.2053" t="0.558"/>\r
+ <eng-data cg="70." f="112.75" m="21.4302" t="0.622"/>\r
+ <eng-data cg="70." f="112.129" m="17.84" t="0.683"/>\r
+ <eng-data cg="70." f="109.125" m="14.5972" t="0.739"/>\r
+ <eng-data cg="70." f="102.017" m="11.4474" t="0.796"/>\r
+ <eng-data cg="70." f="90.494" m="8.07165" t="0.863"/>\r
+ <eng-data cg="70." f="82.75" m="6.34868" t="0.901"/>\r
+ <eng-data cg="70." f="72.41" m="4.96799" t="0.935"/>\r
+ <eng-data cg="70." f="59.869" m="3.54857" t="0.976"/>\r
+ <eng-data cg="70." f="49.826" m="2.34277" t="1.018"/>\r
+ <eng-data cg="70." f="44.321" m="2.09637" t="1.028"/>\r
+ <eng-data cg="70." f="39.805" m="1.78812" t="1.042"/>\r
+ <eng-data cg="70." f="28.272" m="1.23579" t="1.073"/>\r
+ <eng-data cg="70." f="18.231" m="0.748962" t="1.113"/>\r
+ <eng-data cg="70." f="11.176" m="0.310266" t="1.17"/>\r
+ <eng-data cg="70." f="4.636" m="0.111627" t="1.218"/>\r
+ <eng-data cg="70." f="0." m="0." t="1.31"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-;\r
-G125 38.0 408.00 1 0.15800 0.53700 SRS\r
- 0.01 346.87 \r
- 0.04 325.72 \r
- 0.07 324.57 \r
- 0.08 415.57 \r
- 0.09 219.61 \r
- 0.13 194.84 \r
- 0.20 177.77 \r
- 0.40 157.13 \r
- 0.60 131.89 \r
- 0.80 88.31 \r
- 1.00 42.44 \r
- 1.09 14.64 \r
- 1.20 0.00 \r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="97.22" Itot="150.645" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="125.538" burn-time="1.2" cgDiv="10" cgFix="1" cgStep="-1." code="G125" delays="1000" dia="38." exitDia="0." initWt="537." len="408." mDiv="10" mFix="1" mStep="-1." massFrac="29.42" mfg="Sky Ripper Systems" peakThrust="415.57" propWt="158." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+ <eng-data cg="204." f="0." m="158." t="0."/>\r
+ <eng-data cg="204." f="346.87" m="156.181" t="0.01"/>\r
+ <eng-data cg="204." f="325.72" m="145.6" t="0.04"/>\r
+ <eng-data cg="204." f="324.57" m="135.369" t="0.07"/>\r
+ <eng-data cg="204." f="415.57" m="131.488" t="0.08"/>\r
+ <eng-data cg="204." f="219.61" m="128.157" t="0.09"/>\r
+ <eng-data cg="204." f="194.84" m="119.463" t="0.13"/>\r
+ <eng-data cg="204." f="177.77" m="105.785" t="0.2"/>\r
+ <eng-data cg="204." f="157.13" m="70.6599" t="0.4"/>\r
+ <eng-data cg="204." f="131.89" m="40.3469" t="0.6"/>\r
+ <eng-data cg="204." f="88.31" m="17.2519" t="0.8"/>\r
+ <eng-data cg="204." f="42.44" m="3.53851" t="1."/>\r
+ <eng-data cg="204." f="14.64" m="0.844511" t="1.09"/>\r
+ <eng-data cg="204." f="0." m="0." t="1.2"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Sky Ripper Systems 29/75 G63\r
-G63 29 304.80 0 .06500 .23600 SRS\r
- 0.01 121.91 \r
- 0.03 142.66 \r
- 0.07 156.57 \r
- 0.09 133.60 \r
- 0.13 100.62 \r
- 0.18 114.82 \r
- 0.20 105.21 \r
- 0.27 104.91 \r
- 0.35 93.38 \r
- 0.41 83.85 \r
- 0.50 67.95 \r
- 0.65 61.99 \r
- 0.83 61.99 \r
- 0.93 40.14 \r
- 1.09 17.09 \r
- 1.18 13.78 \r
- 1.29 5.56 \r
- 1.30 0.00 \r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="133.21" Itot="84.915" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="65.319" burn-time="1.3" cgDiv="10" cgFix="1" cgStep="-1." code="G63" delays="1000" dia="29." exitDia="0." initWt="236." len="304.8" mDiv="10" mFix="1" mStep="-1." massFrac="27.54" mfg="Sky Ripper Systems" peakThrust="156.57" propWt="65." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <comments>Sky Ripper Systems 29/75 G63</comments>\r
+ <data>\r
+ <eng-data cg="152.4" f="0." m="65." t="0."/>\r
+ <eng-data cg="152.4" f="121.91" m="64.5334" t="0.01"/>\r
+ <eng-data cg="152.4" f="142.66" m="62.5082" t="0.03"/>\r
+ <eng-data cg="152.4" f="156.57" m="57.9272" t="0.07"/>\r
+ <eng-data cg="152.4" f="133.6" m="55.706" t="0.09"/>\r
+ <eng-data cg="152.4" f="100.62" m="52.1202" t="0.13"/>\r
+ <eng-data cg="152.4" f="114.82" m="47.9974" t="0.18"/>\r
+ <eng-data cg="152.4" f="105.21" m="46.3132" t="0.2"/>\r
+ <eng-data cg="152.4" f="104.91" m="40.6837" t="0.27"/>\r
+ <eng-data cg="152.4" f="93.38" m="34.6124" t="0.35"/>\r
+ <eng-data cg="152.4" f="83.85" m="30.5424" t="0.41"/>\r
+ <eng-data cg="152.4" f="67.95" m="25.3135" t="0.5"/>\r
+ <eng-data cg="152.4" f="61.99" m="17.8536" t="0.65"/>\r
+ <eng-data cg="152.4" f="61.99" m="9.31236" t="0.83"/>\r
+ <eng-data cg="152.4" f="40.14" m="5.40349" t="0.93"/>\r
+ <eng-data cg="152.4" f="17.09" m="1.89886" t="1.09"/>\r
+ <eng-data cg="152.4" f="13.78" m="0.83551" t="1.18"/>\r
+ <eng-data cg="152.4" f="5.56" m="0.0212801" t="1.29"/>\r
+ <eng-data cg="152.4" f="0." m="0." t="1.3"/>\r
+ </data>\r
+ </engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;\r
-;Sky Ripper Systems 29/125 G69\r
-G69 29 406.40 0 .10700 .33300 SRS\r
- 0.01 99.80 \r
- 0.04 137.51 \r
- 0.07 103.01 \r
- 0.13 94.13 \r
- 0.30 80.09 \r
- 0.49 72.20 \r
- 0.57 70.72 \r
- 0.65 71.96 \r
- 0.74 80.83 \r
- 0.81 81.81 \r
- 0.94 73.43 \r
- 1.01 74.42 \r
- 1.06 85.02 \r
- 1.11 83.78 \r
- 1.19 62.10 \r
- 1.24 60.62 \r
- 1.32 65.30 \r
- 1.37 64.81 \r
- 1.43 52.98 \r
- 1.49 48.55 \r
- 1.55 44.85 \r
- 1.64 28.59 \r
- 1.85 17.74 \r
- 1.99 14.29 \r
- 2.00 0.00 \r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="121.39" Itot="127.378" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="63.689" burn-time="2." cgDiv="10" cgFix="1" cgStep="-1." code="G69" delays="1000" dia="29." exitDia="0." initWt="333." len="406.4" mDiv="10" mFix="1" mStep="-1." massFrac="32.13" mfg="Sky Ripper Systems" peakThrust="137.51" propWt="107." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+ <comments>Sky Ripper Systems 29/125 G69</comments>\r
+ <data>\r
+ <eng-data cg="203.2" f="0." m="107." t="0."/>\r
+ <eng-data cg="203.2" f="99.8" m="106.581" t="0.01"/>\r
+ <eng-data cg="203.2" f="137.51" m="103.591" t="0.04"/>\r
+ <eng-data cg="203.2" f="103.01" m="100.56" t="0.07"/>\r
+ <eng-data cg="203.2" f="94.13" m="95.5919" t="0.13"/>\r
+ <eng-data cg="203.2" f="80.09" m="83.1523" t="0.3"/>\r
+ <eng-data cg="203.2" f="72.2" m="70.9992" t="0.49"/>\r
+ <eng-data cg="203.2" f="70.72" m="66.197" t="0.57"/>\r
+ <eng-data cg="203.2" f="71.96" m="61.4028" t="0.65"/>\r
+ <eng-data cg="203.2" f="80.83" m="55.6272" t="0.74"/>\r
+ <eng-data cg="203.2" f="81.81" m="50.8455" t="0.81"/>\r
+ <eng-data cg="203.2" f="73.43" m="42.3691" t="0.94"/>\r
+ <eng-data cg="203.2" f="74.42" m="38.0222" t="1.01"/>\r
+ <eng-data cg="203.2" f="85.02" m="34.6739" t="1.06"/>\r
+ <eng-data cg="203.2" f="83.78" m="31.129" t="1.11"/>\r
+ <eng-data cg="203.2" f="62.1" m="26.2273" t="1.19"/>\r
+ <eng-data cg="203.2" f="60.62" m="23.6501" t="1.24"/>\r
+ <eng-data cg="203.2" f="65.3" m="19.4191" t="1.32"/>\r
+ <eng-data cg="203.2" f="64.81" m="16.6867" t="1.37"/>\r
+ <eng-data cg="203.2" f="52.98" m="13.7183" t="1.43"/>\r
+ <eng-data cg="203.2" f="48.55" m="11.1597" t="1.49"/>\r
+ <eng-data cg="203.2" f="44.85" m="8.80596" t="1.55"/>\r
+ <eng-data cg="203.2" f="28.59" m="6.02985" t="1.64"/>\r
+ <eng-data cg="203.2" f="17.74" m="1.94343" t="1.85"/>\r
+ <eng-data cg="203.2" f="14.29" m="0.0600196" t="1.99"/>\r
+ <eng-data cg="203.2" f="0." m="0." t="2."/>\r
+ </data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="134.68" Itot="220.561" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="131.678" burn-time="1.68" cgDiv="10" cgFix="1" cgStep="-1." code="H124" delays="1000" dia="38." exitDia="0." initWt="688." len="608." mDiv="10" mFix="1" mStep="-1." massFrac="24.27" mfg="Sky Ripper Systems" peakThrust="347.884" propWt="167." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Sky Ripper Systems 38mm motor simulation file.\r
+SRS H124 38/220 PVC fuel for Rocksim\r
+</comments>\r
+<data>\r
+<eng-data cg="304." f="0." m="167." t="0."/>\r
+<eng-data cg="304." f="310.274" m="164.063" t="0.025"/>\r
+<eng-data cg="304." f="347.884" m="157.834" t="0.05"/>\r
+<eng-data cg="304." f="310.274" m="151.605" t="0.075"/>\r
+<eng-data cg="304." f="197.447" m="146.8" t="0.1"/>\r
+<eng-data cg="304." f="219.386" m="142.855" t="0.125"/>\r
+<eng-data cg="304." f="200.582" m="138.88" t="0.15"/>\r
+<eng-data cg="304." f="216.252" m="134.935" t="0.175"/>\r
+<eng-data cg="304." f="191.179" m="127.223" t="0.225"/>\r
+<eng-data cg="304." f="216.252" m="123.366" t="0.25"/>\r
+<eng-data cg="304." f="231.922" m="119.125" t="0.275"/>\r
+<eng-data cg="304." f="209.984" m="114.942" t="0.3"/>\r
+<eng-data cg="304." f="184.911" m="111.205" t="0.325"/>\r
+<eng-data cg="304." f="203.716" m="107.527" t="0.35"/>\r
+<eng-data cg="304." f="188.045" m="103.819" t="0.375"/>\r
+<eng-data cg="304." f="162.972" m="97.1744" t="0.425"/>\r
+<eng-data cg="304." f="181.777" m="93.9116" t="0.45"/>\r
+<eng-data cg="304." f="203.716" m="90.2631" t="0.475"/>\r
+<eng-data cg="304." f="206.85" m="86.3773" t="0.5"/>\r
+<eng-data cg="304." f="197.447" m="82.5508" t="0.525"/>\r
+<eng-data cg="304." f="153.57" m="79.2286" t="0.55"/>\r
+<eng-data cg="304." f="184.911" m="76.0251" t="0.575"/>\r
+<eng-data cg="304." f="169.241" m="69.3213" t="0.625"/>\r
+<eng-data cg="304." f="184.911" m="65.9695" t="0.65"/>\r
+<eng-data cg="304." f="181.777" m="62.4989" t="0.675"/>\r
+<eng-data cg="304." f="175.509" m="59.1174" t="0.7"/>\r
+<eng-data cg="304." f="172.375" m="55.8249" t="0.725"/>\r
+<eng-data cg="304." f="162.972" m="52.651" t="0.75"/>\r
+<eng-data cg="304." f="169.241" m="49.5068" t="0.775"/>\r
+<eng-data cg="304." f="131.631" m="43.8116" t="0.825"/>\r
+<eng-data cg="304." f="159.838" m="41.053" t="0.85"/>\r
+<eng-data cg="304." f="178.643" m="37.8494" t="0.875"/>\r
+<eng-data cg="304." f="125.364" m="34.9721" t="0.9"/>\r
+<eng-data cg="304." f="141.034" m="32.4508" t="0.925"/>\r
+<eng-data cg="304." f="115.961" m="30.0185" t="0.95"/>\r
+<eng-data cg="304." f="103.425" m="27.9421" t="0.975"/>\r
+<eng-data cg="304." f="90.8886" m="24.2639" t="1.025"/>\r
+<eng-data cg="304." f="81.4862" m="22.6325" t="1.05"/>\r
+<eng-data cg="304." f="81.4862" m="21.0901" t="1.075"/>\r
+<eng-data cg="304." f="87.7544" m="19.4883" t="1.1"/>\r
+<eng-data cg="304." f="87.7544" m="17.8272" t="1.125"/>\r
+<eng-data cg="304." f="65.8159" m="16.3737" t="1.15"/>\r
+<eng-data cg="304." f="72.0838" m="15.0686" t="1.175"/>\r
+<eng-data cg="304." f="65.8159" m="12.4583" t="1.225"/>\r
+<eng-data cg="304." f="81.4862" m="11.0641" t="1.25"/>\r
+<eng-data cg="304." f="62.6818" m="9.69965" t="1.275"/>\r
+<eng-data cg="304." f="56.4135" m="8.57247" t="1.3"/>\r
+<eng-data cg="304." f="43.8772" m="7.62327" t="1.325"/>\r
+<eng-data cg="304." f="12.5364" m="7.08935" t="1.35"/>\r
+<eng-data cg="304." f="40.7431" m="6.58508" t="1.375"/>\r
+<eng-data cg="304." f="40.7431" m="5.04263" t="1.425"/>\r
+<eng-data cg="304." f="37.609" m="4.30107" t="1.45"/>\r
+<eng-data cg="304." f="34.475" m="3.61883" t="1.475"/>\r
+<eng-data cg="304." f="34.475" m="2.96626" t="1.5"/>\r
+<eng-data cg="304." f="21.9386" m="2.43233" t="1.525"/>\r
+<eng-data cg="304." f="12.5364" m="2.10604" t="1.55"/>\r
+<eng-data cg="304." f="28.2068" m="1.72043" t="1.575"/>\r
+<eng-data cg="304." f="25.0727" m="0.711901" t="1.625"/>\r
+<eng-data cg="304." f="25.0727" m="0.2373" t="1.65"/>\r
+<eng-data cg="304." f="0." m="0." t="1.675"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="136.21" Itot="223.069" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="131.217" burn-time="1.7" cgDiv="10" cgFix="1" cgStep="-1." code="H155" delays="1000" dia="38." exitDia="0." initWt="645." len="508." mDiv="10" mFix="1" mStep="-1." massFrac="25.89" mfg="Sky Ripper Systems" peakThrust="294.604" propWt="167." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>SRS H155 38/220 PP fuel - for Rocksim</comments>\r
+<data>\r
+<eng-data cg="254." f="0." m="167." t="0."/>\r
+<eng-data cg="254." f="266.397" m="164.507" t="0.025"/>\r
+<eng-data cg="254." f="294.604" m="159.257" t="0.05"/>\r
+<eng-data cg="254." f="244.459" m="154.213" t="0.075"/>\r
+<eng-data cg="254." f="219.386" m="149.872" t="0.1"/>\r
+<eng-data cg="254." f="200.582" m="145.942" t="0.125"/>\r
+<eng-data cg="254." f="247.593" m="141.748" t="0.15"/>\r
+<eng-data cg="254." f="269.531" m="136.908" t="0.175"/>\r
+<eng-data cg="254." f="219.386" m="127.758" t="0.225"/>\r
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+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
+++ /dev/null
-;\r
-;Sky Ripper Systems 29/185 H78\r
-H78 29 520.70 0 .15800 .41800 SRS\r
- 0.01 138.21 \r
- 0.08 150.10 \r
- 0.12 142.67 \r
- 0.15 132.27 \r
- 0.22 130.49 \r
- 0.29 90.30 \r
- 0.34 88.27 \r
- 0.40 86.81 \r
- 0.61 86.52 \r
- 0.72 81.59 \r
- 0.76 71.72 \r
- 0.86 64.46 \r
- 1.01 63.30 \r
- 1.18 62.42 \r
- 1.28 60.39 \r
- 1.50 57.49 \r
- 1.80 58.36 \r
- 1.89 59.23 \r
- 2.01 55.46 \r
- 2.21 36.29 \r
- 2.36 22.94 \r
- 2.54 13.36 \r
- 2.72 9.58 \r
- 2.75 0.00 \r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
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+<comments>Sky Ripper Systems 29/185 H78</comments>\r
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+<eng-data cg="260.35" f="0." m="0." t="2.75"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="127.68" Itot="594.768" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="139.945" burn-time="4.25" cgDiv="10" cgFix="1" cgStep="-1." code="I117" delays="1000" dia="38." exitDia="0." initWt="1169." len="914." mDiv="10" mFix="1" mStep="-1." massFrac="40.63" mfg="Sky Ripper Systems" peakThrust="354.151" propWt="475." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>SRS I117 38/580 PVC fuel - for Rocksim</comments>\r
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+<eng-data cg="457." f="0." m="0." t="4.25"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="131.48" Itot="413.882" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="133.51" burn-time="3.1" cgDiv="10" cgFix="1" cgStep="-1." code="I119" delays="1000" dia="38." exitDia="0." initWt="926." len="711." mDiv="10" mFix="1" mStep="-1." massFrac="34.67" mfg="Sky Ripper Systems" peakThrust="304.006" propWt="321." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>SRS I119 38/400 PVC fuel - for Rocksim</comments>\r
+<data>\r
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+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="169.54" Itot="533.709" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="120.612" burn-time="4.42" cgDiv="10" cgFix="1" cgStep="-1." code="I147" delays="1000" dia="38." exitDia="0." initWt="883." len="711." mDiv="10" mFix="1" mStep="-1." massFrac="36.35" mfg="Sky Ripper Systems" peakThrust="497.27" propWt="321." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>SRS I147 38/400 PP fuel - for Rocksim</comments>\r
+<data>\r
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+<eng-data cg="355.5" f="227.625" m="233.053" t="0.6"/>\r
+<eng-data cg="355.5" f="217.607" m="219.664" t="0.7"/>\r
+<eng-data cg="355.5" f="197.85" m="207.17" t="0.8"/>\r
+<eng-data cg="355.5" f="192.285" m="195.438" t="0.9"/>\r
+<eng-data cg="355.5" f="193.676" m="183.59" t="1.00208"/>\r
+<eng-data cg="355.5" f="195.346" m="172.134" t="1.1"/>\r
+<eng-data cg="355.5" f="173.919" m="161.029" t="1.2"/>\r
+<eng-data cg="355.5" f="174.475" m="150.552" t="1.3"/>\r
+<eng-data cg="355.5" f="184.771" m="139.749" t="1.4"/>\r
+<eng-data cg="355.5" f="173.084" m="128.987" t="1.5"/>\r
+<eng-data cg="355.5" f="167.797" m="118.736" t="1.6"/>\r
+<eng-data cg="355.5" f="161.397" m="108.836" t="1.7"/>\r
+<eng-data cg="355.5" f="182.823" m="98.4847" t="1.8"/>\r
+<eng-data cg="355.5" f="168.91" m="87.9072" t="1.9"/>\r
+<eng-data cg="355.5" f="124.387" m="78.9035" t="2.00208"/>\r
+<eng-data cg="355.5" f="132.735" m="71.332" t="2.1"/>\r
+<eng-data cg="355.5" f="136.074" m="63.2483" t="2.2"/>\r
+<eng-data cg="355.5" f="139.97" m="54.9469" t="2.3"/>\r
+<eng-data cg="355.5" f="114.926" m="47.2815" t="2.4"/>\r
+<eng-data cg="355.5" f="101.29" m="40.7793" t="2.5"/>\r
+<eng-data cg="355.5" f="89.8811" m="35.0303" t="2.6"/>\r
+<eng-data cg="355.5" f="70.9588" m="30.1935" t="2.7"/>\r
+<eng-data cg="355.5" f="64.2802" m="26.1265" t="2.8"/>\r
+<eng-data cg="355.5" f="53.428" m="22.5867" t="2.9"/>\r
+<eng-data cg="355.5" f="46.4709" m="19.52" t="3.00208"/>\r
+<eng-data cg="355.5" f="44.8013" m="16.8323" t="3.1"/>\r
+<eng-data cg="355.5" f="39.5143" m="14.2967" t="3.2"/>\r
+<eng-data cg="355.5" f="33.6707" m="12.0958" t="3.3"/>\r
+<eng-data cg="355.5" f="29.7749" m="10.1879" t="3.4"/>\r
+<eng-data cg="355.5" f="27.2704" m="8.47237" t="3.5"/>\r
+<eng-data cg="355.5" f="22.8181" m="6.96608" t="3.6"/>\r
+<eng-data cg="355.5" f="20.0354" m="5.67736" t="3.7"/>\r
+<eng-data cg="355.5" f="17.531" m="4.54764" t="3.8"/>\r
+<eng-data cg="355.5" f="16.9745" m="3.50997" t="3.9"/>\r
+<eng-data cg="355.5" f="15.0266" m="2.5276" t="4.00208"/>\r
+<eng-data cg="355.5" f="11.1308" m="1.75734" t="4.1"/>\r
+<eng-data cg="355.5" f="9.73945" m="1.12972" t="4.2"/>\r
+<eng-data cg="355.5" f="9.73945" m="0.543939" t="4.3"/>\r
+<eng-data cg="355.5" f="6.67847" m="0.0502097" t="4.4"/>\r
+<eng-data cg="355.5" f="0." m="0." t="4.425"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="137.96" Itot="642.634" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="110.799" burn-time="5.8" cgDiv="10" cgFix="1" cgStep="-1." code="J144" delays="1000" dia="38." exitDia="0." initWt="1126." len="914." mDiv="10" mFix="1" mStep="-1." massFrac="42.18" mfg="Sky Ripper Systems" peakThrust="327.245" propWt="475." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>SRS J144 38/580 PP fuel - for Rocksim</comments>\r
+<data>\r
+<eng-data cg="457." f="0." m="475." t="0."/>\r
+<eng-data cg="457." f="327.245" m="471.976" t="0.025"/>\r
+<eng-data cg="457." f="247.938" m="456.034" t="0.1"/>\r
+<eng-data cg="457." f="261.296" m="437.214" t="0.2"/>\r
+<eng-data cg="457." f="293.018" m="416.728" t="0.3"/>\r
+<eng-data cg="457." f="255.452" m="396.458" t="0.4"/>\r
+<eng-data cg="457." f="247.66" m="377.864" t="0.5"/>\r
+<eng-data cg="457." f="240.982" m="359.805" t="0.6"/>\r
+<eng-data cg="457." f="235.973" m="342.178" t="0.7"/>\r
+<eng-data cg="457." f="228.181" m="325.024" t="0.8"/>\r
+<eng-data cg="457." f="205.92" m="308.981" t="0.9"/>\r
+<eng-data cg="457." f="193.119" m="293.927" t="1.00208"/>\r
+<eng-data cg="457." f="175.032" m="280.604" t="1.1"/>\r
+<eng-data cg="457." f="183.101" m="267.369" t="1.2"/>\r
+<eng-data cg="457." f="176.701" m="254.071" t="1.3"/>\r
+<eng-data cg="457." f="172.249" m="241.175" t="1.4"/>\r
+<eng-data cg="457." f="170.301" m="228.515" t="1.5"/>\r
+<eng-data cg="457." f="168.075" m="216.01" t="1.6"/>\r
+<eng-data cg="457." f="157.223" m="203.988" t="1.7"/>\r
+<eng-data cg="457." f="152.77" m="192.531" t="1.8"/>\r
+<eng-data cg="457." f="156.11" m="181.116" t="1.9"/>\r
+<eng-data cg="457." f="156.11" m="169.337" t="2.00208"/>\r
+<eng-data cg="457." f="148.874" m="158.3" t="2.1"/>\r
+<eng-data cg="457." f="137.744" m="147.707" t="2.2"/>\r
+<eng-data cg="457." f="139.135" m="137.475" t="2.3"/>\r
+<eng-data cg="457." f="130.23" m="127.52" t="2.4"/>\r
+<eng-data cg="457." f="128.004" m="117.976" t="2.5"/>\r
+<eng-data cg="457." f="128.004" m="108.515" t="2.6"/>\r
+<eng-data cg="457." f="137.465" m="98.7037" t="2.7"/>\r
+<eng-data cg="457." f="112.977" m="89.4481" t="2.8"/>\r
+<eng-data cg="457." f="130.787" m="80.4392" t="2.9"/>\r
+<eng-data cg="457." f="106.299" m="71.4949" t="3.00208"/>\r
+<eng-data cg="457." f="96.003" m="64.1739" t="3.1"/>\r
+<eng-data cg="457." f="84.5941" m="57.4995" t="3.2"/>\r
+<eng-data cg="457." f="80.42" m="51.401" t="3.3"/>\r
+<eng-data cg="457." f="70.124" m="45.8373" t="3.4"/>\r
+<eng-data cg="457." f="62.0544" m="40.9524" t="3.5"/>\r
+<eng-data cg="457." f="59.5499" m="36.4582" t="3.6"/>\r
+<eng-data cg="457." f="53.428" m="32.2829" t="3.7"/>\r
+<eng-data cg="457." f="45.6361" m="28.6217" t="3.8"/>\r
+<eng-data cg="457." f="42.5753" m="25.3617" t="3.9"/>\r
+<eng-data cg="457." f="37.5665" m="22.3382" t="4.00208"/>\r
+<eng-data cg="457." f="32.8358" m="19.7905" t="4.1"/>\r
+<eng-data cg="457." f="31.7228" m="17.4046" t="4.2"/>\r
+<eng-data cg="457." f="27.827" m="15.2038" t="4.3"/>\r
+<eng-data cg="457." f="23.9312" m="13.2909" t="4.4"/>\r
+<eng-data cg="457." f="23.3747" m="11.5426" t="4.5"/>\r
+<eng-data cg="457." f="20.0354" m="9.9383" t="4.6"/>\r
+<eng-data cg="457." f="17.8093" m="8.53966" t="4.7"/>\r
+<eng-data cg="457." f="16.1397" m="7.285" t="4.8"/>\r
+<eng-data cg="457." f="15.3048" m="6.12289" t="4.9"/>\r
+<eng-data cg="457." f="13.0787" m="5.0521" t="5.00208"/>\r
+<eng-data cg="457." f="10.296" m="4.2062" t="5.1"/>\r
+<eng-data cg="457." f="11.1308" m="3.41432" t="5.2"/>\r
+<eng-data cg="457." f="8.90463" m="2.67387" t="5.3"/>\r
+<eng-data cg="457." f="8.62637" m="2.02597" t="5.4"/>\r
+<eng-data cg="457." f="7.23503" m="1.43978" t="5.5"/>\r
+<eng-data cg="457." f="8.62637" m="0.853581" t="5.6"/>\r
+<eng-data cg="457." f="7.23503" m="0.267387" t="5.7"/>\r
+<eng-data cg="457." f="0." m="0." t="5.8"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="West Coast Hybrids" code="G55" Type="hybrid" dia="38." len="308."\r
+initWt="465.8" propWt="140.8" delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="48.019" peakThrust="144.052" throatDia="0." exitDia="0."\r
+Itot="150.683" burn-time="3.14" massFrac="30.23" Isp="109.13" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+ <comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve and engine data from C.A.R. certification dated\r
+June 8, 2006.\r
+</comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="140.8" cg="154."/>\r
+ <eng-data t="0.053" f="144.052" m="137.233" cg="154."/>\r
+ <eng-data t="0.124" f="75.173" m="129.961" cg="154."/>\r
+ <eng-data t="0.212" f="73.425" m="123.851" cg="154."/>\r
+ <eng-data t="0.313" f="70.977" m="117.037" cg="154."/>\r
+ <eng-data t="0.649" f="62.936" m="96.0155" cg="154."/>\r
+ <eng-data t="0.879" f="57.341" m="83.0908" cg="154."/>\r
+ <eng-data t="1.02" f="55.243" m="75.6742" cg="154."/>\r
+ <eng-data t="1.162" f="54.194" m="68.4138" cg="154."/>\r
+ <eng-data t="1.239" f="56.992" m="64.4139" cg="154."/>\r
+ <eng-data t="1.498" f="54.194" m="50.9597" cg="154."/>\r
+ <eng-data t="1.539" f="51.397" m="48.937" cg="154."/>\r
+ <eng-data t="1.634" f="49.999" m="44.4366" cg="154."/>\r
+ <eng-data t="1.693" f="52.097" m="41.6223" cg="154."/>\r
+ <eng-data t="1.822" f="51.747" m="35.3636" cg="154."/>\r
+ <eng-data t="1.899" f="49.999" m="31.7033" cg="154."/>\r
+ <eng-data t="2.047" f="48.251" m="24.9097" cg="154."/>\r
+ <eng-data t="2.094" f="46.153" m="22.8367" cg="154."/>\r
+ <eng-data t="2.17" f="39.859" m="19.7826" cg="154."/>\r
+ <eng-data t="2.247" f="36.363" m="17.0405" cg="154."/>\r
+ <eng-data t="2.577" f="22.377" m="7.98407" cg="154."/>\r
+ <eng-data t="2.955" f="15.384" m="1.31532" cg="154."/>\r
+ <eng-data t="3.138" f="0." m="0." cg="154."/>\r
+ </data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="West Coast Hybrids" code="H100" Type="hybrid" dia="38." len="403."\r
+initWt="450." propWt="95." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="85.301" peakThrust="169.257" throatDia="0." exitDia="0."\r
+Itot="213.252" burn-time="2.5" massFrac="21.11" Isp="228.9" tDiv="10" tStep="-1."\r
+tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve and engine data from C.A.R. certification dated\r
+10-29-04.\r
+</comments>\r
+<data>\r
+ <eng-data t="0." f="0." m="95." cg="201.5"/>\r
+ <eng-data t="0.017" f="32.438" m="94.8772" cg="201.5"/>\r
+ <eng-data t="0.168" f="167.972" m="88.1366" cg="201.5"/>\r
+ <eng-data t="0.206" f="169.257" m="85.2822" cg="201.5"/>\r
+ <eng-data t="0.217" f="166.688" m="84.4591" cg="201.5"/>\r
+ <eng-data t="0.324" f="139.709" m="77.1567" cg="201.5"/>\r
+ <eng-data t="0.423" f="137.14" m="71.0518" cg="201.5"/>\r
+ <eng-data t="0.484" f="134.571" m="67.36" cg="201.5"/>\r
+ <eng-data t="0.548" f="130.395" m="63.5828" cg="201.5"/>\r
+ <eng-data t="0.582" f="127.184" m="61.6321" cg="201.5"/>\r
+ <eng-data t="0.643" f="125.257" m="58.2021" cg="201.5"/>\r
+ <eng-data t="1.002" f="114.979" m="38.9919" cg="201.5"/>\r
+ <eng-data t="1.037" f="114.337" m="37.2042" cg="201.5"/>\r
+ <eng-data t="1.092" f="114.016" m="34.4067" cg="201.5"/>\r
+ <eng-data t="1.159" f="113.052" m="31.018" cg="201.5"/>\r
+ <eng-data t="1.243" f="108.556" m="26.8717" cg="201.5"/>\r
+ <eng-data t="1.269" f="104.702" m="25.6366" cg="201.5"/>\r
+ <eng-data t="1.335" f="96.673" m="22.6762" cg="201.5"/>\r
+ <eng-data t="1.373" f="93.461" m="21.0669" cg="201.5"/>\r
+ <eng-data t="1.408" f="91.855" m="19.6222" cg="201.5"/>\r
+ <eng-data t="1.472" f="89.607" m="17.0354" cg="201.5"/>\r
+ <eng-data t="1.512" f="86.395" m="15.4673" cg="201.5"/>\r
+ <eng-data t="1.547" f="82.862" m="14.1478" cg="201.5"/>\r
+ <eng-data t="1.582" f="77.723" m="12.8958" cg="201.5"/>\r
+ <eng-data t="1.75" f="54.92" m="7.93228" cg="201.5"/>\r
+ <eng-data t="1.868" f="41.431" m="5.39985" cg="201.5"/>\r
+ <eng-data t="2.071" f="25.051" m="2.39377" cg="201.5"/>\r
+ <eng-data t="2.5" f="0." m="0." cg="201.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="West Coast Hybrids" code="I110" Type="hybrid" dia="38." len="606."\r
+initWt="824." propWt="327." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="112.605" peakThrust="240." throatDia="0." exitDia="0." Itot="450.42"\r
+burn-time="4." massFrac="39.68" Isp="140.46" tDiv="10" tStep="-1." tFix="1"\r
+FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+ <comments><![CDATA[based on CAR thrust curve & cert letter\r
+received from WestCoast/Scott Harrison\r
+compiled by RockSim EngEdit\r
+hand entered data points from CAR thrust curve\r
+approx 10% higher total impulse than cert letter\r
+approx 5% higher total impulse than thrust curve\r
+within a couple percent for peak & average thrust\r
+accurate thrust profile\r
+Andrew MacMillen NAR 77472 8/8/02\r
+NOTE: NOT WCH, CAR, TMT OR NAR APPROVED\r
+West Coast Hybrids I110\r
+]]></comments>\r
+ <data>\r
+ <eng-data t="0." f="0." m="327." cg="303."/>\r
+ <eng-data t="0.05" f="240." m="322.644" cg="303."/>\r
+ <eng-data t="0.38" f="200." m="269.937" cg="303."/>\r
+ <eng-data t="0.76" f="182." m="217.245" cg="303."/>\r
+ <eng-data t="1.14" f="160." m="170.07" cg="303."/>\r
+ <eng-data t="1.52" f="142." m="128.413" cg="303."/>\r
+ <eng-data t="1.9" f="125." m="91.5835" cg="303."/>\r
+ <eng-data t="2.23" f="113." m="63.0739" cg="303."/>\r
+ <eng-data t="2.66" f="71." m="34.3538" cg="303."/>\r
+ <eng-data t="3.04" f="44." m="18.4909" cg="303."/>\r
+ <eng-data t="3.42" f="29." m="8.42147" cg="303."/>\r
+ <eng-data t="3.78" f="22." m="1.75689" cg="303."/>\r
+ <eng-data t="4." f="0." m="0." cg="303."/>\r
+ </data>\r
+ </engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="West Coast Hybrids" code="K460" Type="hybrid" dia="75." len="762."\r
+initWt="3650." propWt="1360." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="440.282" peakThrust="789.754" throatDia="0." exitDia="0."\r
+Itot="1761.13" burn-time="4." massFrac="37.26" Isp="132.05" tDiv="10" tStep="-1."\r
+tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve and engine data from C.A.R. certification dated\r
+3-5-05.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="1360." cg="381."/>\r
+<eng-data t="0.048" f="263.772" m="1355.11" cg="381."/>\r
+<eng-data t="0.181" f="789.754" m="1301.01" cg="381."/>\r
+<eng-data t="0.21" f="769.464" m="1283.55" cg="381."/>\r
+<eng-data t="0.229" f="728.884" m="1272.56" cg="381."/>\r
+<eng-data t="0.31" f="711.715" m="1227.5" cg="381."/>\r
+<eng-data t="0.344" f="694.547" m="1209.04" cg="381."/>\r
+<eng-data t="0.368" f="672.696" m="1196.37" cg="381."/>\r
+<eng-data t="0.411" f="658.649" m="1174.27" cg="381."/>\r
+<eng-data t="0.477" f="638.359" m="1141.21" cg="381."/>\r
+<eng-data t="0.535" f="625.872" m="1112.9" cg="381."/>\r
+<eng-data t="0.573" f="618.068" m="1094.65" cg="381."/>\r
+<eng-data t="0.601" f="607.143" m="1081.4" cg="381."/>\r
+<eng-data t="0.764" f="496.328" m="1011.96" cg="381."/>\r
+<eng-data t="0.792" f="483.841" m="1001.36" cg="381."/>\r
+<eng-data t="0.826" f="477.598" m="988.737" cg="381."/>\r
+<eng-data t="0.964" f="458.869" m="938.838" cg="381."/>\r
+<eng-data t="1.093" f="429.214" m="894.604" cg="381."/>\r
+<eng-data t="1.232" f="533.786" m="842.92" cg="381."/>\r
+<eng-data t="1.27" f="563.441" m="826.821" cg="381."/>\r
+<eng-data t="1.298" f="602.461" m="814.216" cg="381."/>\r
+<eng-data t="1.356" f="613.386" m="786.987" cg="381."/>\r
+<eng-data t="1.432" f="630.555" m="750.484" cg="381."/>\r
+<eng-data t="1.489" f="628.994" m="722.763" cg="381."/>\r
+<eng-data t="1.551" f="619.629" m="692.872" cg="381."/>\r
+<eng-data t="1.599" f="614.947" m="669.991" cg="381."/>\r
+<eng-data t="1.642" f="616.508" m="649.545" cg="381."/>\r
+<eng-data t="1.718" f="633.676" m="612.859" cg="381."/>\r
+<eng-data t="1.8" f="643.041" m="572.436" cg="381."/>\r
+<eng-data t="1.857" f="657.088" m="543.822" cg="381."/>\r
+<eng-data t="1.895" f="653.966" m="524.586" cg="381."/>\r
+<eng-data t="1.957" f="669.574" m="492.901" cg="381."/>\r
+<eng-data t="2.019" f="677.378" m="460.656" cg="381."/>\r
+<eng-data t="2.081" f="677.378" m="428.224" cg="381."/>\r
+<eng-data t="2.153" f="652.406" m="391.256" cg="381."/>\r
+<eng-data t="2.277" f="607.143" m="330.951" cg="381."/>\r
+<eng-data t="2.396" f="575.927" m="276.591" cg="381."/>\r
+<eng-data t="2.477" f="558.759" m="241.104" cg="381."/>\r
+<eng-data t="2.525" f="549.394" m="220.566" cg="381."/>\r
+<eng-data t="2.597" f="510.375" m="191.104" cg="381."/>\r
+<eng-data t="2.678" f="437.018" m="161.474" cg="381."/>\r
+<eng-data t="2.764" f="363.661" m="134.886" cg="381."/>\r
+<eng-data t="2.883" f="285.623" m="105.053" cg="381."/>\r
+<eng-data t="3.141" f="181.05" m="58.564" cg="381."/>\r
+<eng-data t="3.341" f="124.862" m="34.9405" cg="381."/>\r
+<eng-data t="3.728" f="63.992" m="6.72067" cg="381."/>\r
+<eng-data t="4." f="0." m="0." cg="381."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+ <engine mfg="West Coast Hybrids" code="L600" Type="hybrid" dia="75." len="1016."\r
+initWt="5134." propWt="2265." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="583.141" peakThrust="1148.36" throatDia="0." exitDia="0."\r
+Itot="3174.03" burn-time="5.44" massFrac="44.12" Isp="142.9" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve and engine data from C.A.R. certification dated\r
+6-30-06.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="2265." cg="508."/>\r
+<eng-data t="0.072" f="871.284" m="2242.62" cg="508."/>\r
+<eng-data t="0.119" f="580.856" m="2218.27" cg="508."/>\r
+<eng-data t="0.215" f="674.327" m="2175.27" cg="508."/>\r
+<eng-data t="0.263" f="564.164" m="2154.06" cg="508."/>\r
+<eng-data t="0.31" f="704.371" m="2132.79" cg="508."/>\r
+<eng-data t="0.43" f="831.225" m="2067.04" cg="508."/>\r
+<eng-data t="0.477" f="787.827" m="2039.89" cg="508."/>\r
+<eng-data t="0.561" f="1148.36" m="1981.86" cg="508."/>\r
+<eng-data t="0.633" f="1098.29" m="1924.14" cg="508."/>\r
+<eng-data t="0.752" f="1124.99" m="1829.74" cg="508."/>\r
+<eng-data t="0.883" f="1101.62" m="1725.67" cg="508."/>\r
+<eng-data t="0.979" f="804.519" m="1660.38" cg="508."/>\r
+<eng-data t="1.134" f="761.121" m="1573.79" cg="508."/>\r
+<eng-data t="1.241" f="847.916" m="1512.36" cg="508."/>\r
+<eng-data t="1.337" f="767.798" m="1457.02" cg="508."/>\r
+<eng-data t="1.42" f="754.445" m="1411.94" cg="508."/>\r
+<eng-data t="1.468" f="774.474" m="1385.75" cg="508."/>\r
+<eng-data t="1.552" f="744.43" m="1340.23" cg="508."/>\r
+<eng-data t="1.946" f="711.048" m="1135.62" cg="508."/>\r
+<eng-data t="2.626" f="684.342" m="797.064" cg="508."/>\r
+<eng-data t="3.056" f="674.327" m="588.611" cg="508."/>\r
+<eng-data t="3.39" f="614.238" m="435.05" cg="508."/>\r
+<eng-data t="3.473" f="630.93" m="398.175" cg="508."/>\r
+<eng-data t="3.593" f="627.591" m="344.29" cg="508."/>\r
+<eng-data t="3.724" f="610.9" m="286.402" cg="508."/>\r
+<eng-data t="3.796" f="574.179" m="255.958" cg="508."/>\r
+<eng-data t="3.927" f="450.664" m="208.055" cg="508."/>\r
+<eng-data t="4.058" f="380.561" m="169.203" cg="508."/>\r
+<eng-data t="4.393" f="257.045" m="92.9911" cg="508."/>\r
+<eng-data t="4.727" f="166.913" m="42.4673" cg="508."/>\r
+<eng-data t="5.168" f="63.427" m="6.22348" cg="508."/>\r
+<eng-data t="5.443" f="0." m="0." cg="508."/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine mfg="West Coast Hybrids" code="M700" Type="hybrid" dia="75." len="1473."\r
+initWt="7268." propWt="3043." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="663.477" peakThrust="1256.94" throatDia="0." exitDia="0."\r
+Itot="5598.42" burn-time="8.44" massFrac="41.87" Isp="187.6" tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
+Tracer program. Thrust curve and engine data from C.A.R. certification dated\r
+5-30-06.\r
+</comments>\r
+<data>\r
+<eng-data t="0." f="0." m="3043." cg="736.5"/>\r
+<eng-data t="0.06" f="387.313" m="3036.68" cg="736.5"/>\r
+<eng-data t="0.12" f="931.743" m="3015.18" cg="736.5"/>\r
+<eng-data t="0.215" f="1004.82" m="2965.18" cg="736.5"/>\r
+<eng-data t="0.251" f="1256.94" m="2943.05" cg="736.5"/>\r
+<eng-data t="0.394" f="1253.29" m="2845.49" cg="736.5"/>\r
+<eng-data t="0.49" f="1023.09" m="2786.1" cg="736.5"/>\r
+<eng-data t="0.645" f="869.627" m="2706.37" cg="736.5"/>\r
+<eng-data t="0.765" f="964.628" m="2646.55" cg="736.5"/>\r
+<eng-data t="0.813" f="825.78" m="2623.19" cg="736.5"/>\r
+<eng-data t="1.028" f="781.934" m="2529.25" cg="736.5"/>\r
+<eng-data t="1.183" f="898.858" m="2458.45" cg="736.5"/>\r
+<eng-data t="1.41" f="902.512" m="2347.32" cg="736.5"/>\r
+<eng-data t="1.924" f="909.82" m="2094.15" cg="736.5"/>\r
+<eng-data t="2.295" f="858.665" m="1915.84" cg="736.5"/>\r
+<eng-data t="2.51" f="855.011" m="1815.71" cg="736.5"/>\r
+<eng-data t="2.773" f="869.627" m="1692.44" cg="736.5"/>\r
+<eng-data t="2.976" f="898.858" m="1594.87" cg="736.5"/>\r
+<eng-data t="3.43" f="880.589" m="1375.31" cg="736.5"/>\r
+<eng-data t="4.231" f="829.434" m="1003.06" cg="736.5"/>\r
+<eng-data t="5.187" f="760.01" m="590.095" cg="736.5"/>\r
+<eng-data t="5.378" f="738.087" m="512.33" cg="736.5"/>\r
+<eng-data t="5.558" f="712.51" m="441.368" cg="736.5"/>\r
+<eng-data t="5.677" f="679.624" m="396.345" cg="736.5"/>\r
+<eng-data t="5.833" f="595.585" m="342.281" cg="736.5"/>\r
+<eng-data t="5.952" f="526.161" m="306.002" cg="736.5"/>\r
+<eng-data t="6.263" f="405.582" m="227.25" cg="736.5"/>\r
+<eng-data t="6.884" f="270.388" m="113.166" cg="736.5"/>\r
+<eng-data t="7.542" f="153.464" m="37.3698" cg="736.5"/>\r
+<eng-data t="8.438" f="0." m="0." cg="736.5"/>\r
+</data>\r
+</engine>\r
+</engine-list>\r
+</engine-database>\r
+++ /dev/null
-AeroTech_G339.eng
-AeroTech_G69.eng
-AeroTech_H112.eng
-AeroTech_H123.eng
-AeroTech_H148.eng
-AeroTech_H165.eng
-AeroTech_H210.eng
-AeroTech_H242_1.eng
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-AeroTech_H45.eng
-AeroTech_H55.eng
-AeroTech_H669.eng
-AeroTech_H70.eng
-AeroTech_H999.eng
-AeroTech_I132.eng
-AeroTech_I154.eng
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-AeroTech_I195_1.eng
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-AeroTech_I285.eng
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-AeroTech_I435_1.eng
-AeroTech_I65.eng
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-AeroTech_K458.eng
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-AeroTech_K550.eng
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-AeroTech_K695.eng
-AeroTech_K700.eng
-AeroTech_K780.eng
-AeroTech_L1120.eng
-AeroTech_L1150.eng
-AeroTech_L1500.eng
-AeroTech_L850.eng
-AeroTech_L952.eng
-AeroTech_M1297.eng
-AeroTech_M1315.eng
-AeroTech_M1419.eng
-AeroTech_M1550.eng
-AeroTech_M1600.eng
-AeroTech_M1850.eng
-AeroTech_M1939.eng
-AeroTech_M2000.eng
-AeroTech_M2400.eng
-AeroTech_M2500.eng
-AeroTech_M650.eng
-AeroTech_M750.eng
-AeroTech_N2000.eng
-AeroTech_N4800.eng
-AMW_I271.eng
-AMW_I285.eng
-AMW_J357.eng
-AMW_J365.eng
-AMW_J450_1.eng
-AMW_K555.eng
-AMW_K570.eng
-AMW_K600_1.eng
-AMW_K650.eng
-AMW_K670_1.eng
-AMW_K800.eng
-AMW_K950_1.eng
-AMW_K975.eng
-AMW_L1060_1.eng
-AMW_L666.eng
-AMW_L777_1.eng
-AMW_M1350.eng
-AMW_M1730.eng
-AMW_M1850_1.eng
-AMW_M1850.eng
-AMW_M2500.eng
-AMW_M3000.eng
-AMW_N2020.eng
-AMW_N4000.eng
-Cesaroni_G60.eng
-Cesaroni_I170.eng
-Cesaroni_I240.eng
-Cesaroni_J300.eng
-Cesaroni_J360.eng
-Cesaroni_K510_1.eng
-Cesaroni_K510.eng
-Cesaroni_L1115_1.eng
-Cesaroni_L1115.eng
-Cesaroni_L610.eng
-Cesaroni_L730.eng
-Cesaroni_L800_1.eng
-Cesaroni_L800.eng
-Cesaroni_M1060.eng
-Cesaroni_M1400_1.eng
-Cesaroni_M1400.eng
-Cesaroni_M1450.eng
-Cesaroni_M2505.eng
-Cesaroni_M520.eng
-Cesaroni_M795.eng
-Cesaroni_N1100.eng
-Cesaroni_N2500.eng
-Contrail_G100.eng
-Contrail_G123.eng
-Contrail_G130.eng
-Contrail_G234.eng
-Contrail_G300.eng
-Contrail_H121.eng
-Contrail_H141.eng
-Contrail_H211.eng
-Contrail_H222.eng
-Contrail_H246.eng
-Contrail_H277.eng
-Contrail_H300.eng
-Contrail_H303.eng
-Contrail_H340.eng
-Contrail_I155.eng
-Contrail_I210.eng
-Contrail_I221.eng
-Contrail_I290.eng
-Contrail_I307.eng
-Contrail_I333.eng
-Contrail_I400.eng
-Contrail_I500.eng
-Contrail_I727.eng
-Contrail_I747.eng
-Contrail_J150.eng
-Contrail_J222.eng
-Contrail_J234.eng
-Contrail_J242.eng
-Contrail_J245.eng
-Contrail_J246.eng
-Contrail_J272.eng
-Contrail_J292.eng
-Contrail_J333.eng
-Contrail_J345.eng
-Contrail_J355.eng
-Contrail_J358.eng
-Contrail_J416.eng
-Contrail_J555.eng
-Contrail_J642.eng
-Contrail_J800.eng
-Contrail_K234.eng
-Contrail_K265.eng
-Contrail_K300.eng
-Contrail_K321.eng
-Contrail_K404.eng
-Contrail_K456.eng
-Contrail_K630.eng
-Contrail_K678.eng
-Contrail_K707.eng
-Contrail_K777.eng
-Contrail_L1222.eng
-Contrail_L2525.eng
-Contrail_L369.eng
-Contrail_L800.eng
-Contrail_M1575.eng
-Contrail_M2700.eng
-Contrail_M2800.eng
-Contrail_M711.eng
-Contrail_O6300.eng
-Ellis_I150.eng
-Ellis_I160.eng
-Ellis_I230.eng
-Ellis_J270.eng
-Ellis_J330.eng
-Ellis_L330.eng
-Ellis_L600.eng
-Ellis_M1000.eng
-Estes_B6.eng
-Estes_E9.eng
-Hypertek_I310.eng
-Hypertek_J115.eng
-Hypertek_J120.eng
-Hypertek_J150.eng
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-Hypertek_J190.eng
-Hypertek_J220.eng
-Hypertek_J250_1.eng
-Hypertek_J250.eng
-Hypertek_J270.eng
-Hypertek_J317.eng
-Hypertek_J330_1.eng
-Hypertek_J330.eng
-Hypertek_K240.eng
-Hypertek_L200.eng
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-Hypertek_L350.eng
-Hypertek_L355.eng
-Hypertek_L475.eng
-Hypertek_L535.eng
-Hypertek_L540_1.eng
-Hypertek_L540.eng
-Hypertek_L550.eng
-Hypertek_L570_1.eng
-Hypertek_L570.eng
-Hypertek_L575_1.eng
-Hypertek_L575.eng
-Hypertek_L610.eng
-Hypertek_L625_1.eng
-Hypertek_L625.eng
-Hypertek_M1000_1.eng
-Hypertek_M1000.eng
-Hypertek_M1010_1.eng
-Hypertek_M1010.eng
-KBA_K1750.eng
-KBA_K600.eng
-KBA_K750.eng
-KBA_L1000.eng
-KBA_M1450.eng
-Loki_J525.eng
-Loki_K250.eng
-Loki_K350.eng
-Loki_K960.eng
-Loki_L1400.eng
-Loki_L930.eng
-Loki_M1882.eng
-Quest_C6.eng
-Quest_D5.eng
-RATT_H70.eng
-RATT_I80.eng
-RATT_I90.eng
-RATT_K240.eng
-SkyR_G63.eng
-SkyR_G69.eng
-SkyR_H124.eng
-SkyR_H155.eng
-SkyR_H78.eng
-SkyR_I117.eng
-SkyR_I119.eng
-SkyR_I147.eng
-SkyR_J144.eng
-SkyR_J261.eng
-SkyR_J263.eng
-SkyR_J337.eng
-SkyR_J348.eng
-SkyR_K257.eng
-SkyR_K347.eng
-WCH_I110.eng
// TODO: HIGH: loading the thrust curves and other databases
static {
-
+ final String filePattern = ".*\\.([eE][nN][gG]|[rR][sS][eE])$";
try {
- MOTOR.loadJarDirectory("datafiles/thrustcurves/", ".*\\.[eE][nN][gG]$");
+ MOTOR.loadJarDirectory("datafiles/thrustcurves/", filePattern);
} catch (IOException e) {
System.out.println("Could not read thrust curves from JAR: "+e.getMessage());
}
try {
- MOTOR.loadDirectory(dir, ".*\\.[eE][nN][gG]$");
+ MOTOR.loadDirectory(dir, filePattern);
} catch (IOException e1) {
System.out.println("Could not read thrust curves from directory either.");
throw new ConfigurationException("Couldn't read thrust curves from either " +
if (propW > totalW) {
throw new IOException("Propellant weight exceeds total weight in " +
- "RASP file");
+ "RASP file " + filename);
}
// Read the data
if (row >= 0) {
row = table.convertRowIndexToModel(row);
Motor m = model.getMotor(row);
+ // TODO: HIGH: equals or == ?
if (!m.equals(selectedMotor)) {
selectedMotor = model.getMotor(row);
setDelays(true); // Reset delay times
private static void runMain(String[] args) {
+ // Initialize the splash screen with version info
+ Splash.init();
+
+
// Start update info fetching
final UpdateInfoRetriever updateInfo;
if (Prefs.getCheckUpdates()) {
if (data==null)
return null;
-
- // TODO: CRITICAL: Show getMaxAcceleration if branches not available!
return UnitGroup.UNITS_ACCELERATION.getDefaultUnit().toStringUnit(
data.getMaxAcceleration());
}
manufacturers.add(new Manufacturer("Cesaroni Technology Inc.",
"Cesaroni Technology",
"CES", "CESARONI", "CESARONI TECHNOLOGY INCORPORATED", "CTI",
- "CS", "CSR", "PRO38"));
+ "CS", "CSR", "PRO38", "ABC"));
manufacturers.add(new Manufacturer("Contrail Rockets","Contrail Rockets",
"CR", "CONTR", "CONTRAIL", "CONTRAIL ROCKET"));
package net.sf.openrocket.motor;
import java.text.Collator;
+import java.util.Arrays;
import java.util.Comparator;
import java.util.Locale;
import java.util.regex.Matcher;
this.description = description.trim();
this.motorType = type;
this.delays = delays.clone();
+ Arrays.sort(this.delays);
this.diameter = diameter;
this.length = length;
this.digest = digest;
}
+ public boolean similar(Motor other) {
+ // TODO: HIGH: Merge with equals / cleanup
+
+ // Tests manufacturer, designation, diameter and length
+ if (this.compareTo(other) != 0)
+ return false;
+
+ // Compare total time
+ if (Math.abs(this.getTotalTime() - other.getTotalTime()) > 0.5) {
+ return false;
+ }
+
+ // Consider type only if neither is of unknown type
+ if ((this.motorType != Type.UNKNOWN) && (other.motorType != Type.UNKNOWN) &&
+ (this.motorType != other.motorType)) {
+ return false;
+ }
+
+ // Compare delays if both have some delays defined
+ if (this.delays.length != 0 && other.delays.length != 0) {
+ if (this.delays.length != other.delays.length) {
+ return false;
+ }
+ for (int i=0; i < delays.length; i++) {
+ // INF - INF == NaN, which produces false when compared
+ if (Math.abs(this.delays[i] - other.delays[i]) > 0.5) {
+ return false;
+ }
+ }
+ }
+
+ double time = getTotalTime();
+ for (int i=0; i < 10; i++) {
+ double t = time * i/10;
+ if (Math.abs(this.getThrust(t) - other.getThrust(t)) > 1) {
+ return false;
+ }
+ }
+
+ return true;
+ }
+
/**
* Compares two <code>Motor</code> objects. The motors are considered equal
* if they have identical manufacturers, designations and types, near-identical
* (sampled at 10 equidistant points).
* <p>
* The comment field is ignored when comparing equality.
+ * <p>
+ * TODO: HIGH: Check for identical contents instead
*/
@Override
public boolean equals(Object o) {
if (this.compareTo(other) != 0)
return false;
- if (Math.abs(this.getTotalTime() - other.getTotalTime()) > 0.5 ||
- this.motorType != other.motorType ||
- this.delays.length != other.delays.length) {
-
+ // Compare total time
+ if (Math.abs(this.getTotalTime() - other.getTotalTime()) > 0.5) {
return false;
}
+ // Consider type only if neither is of unknown type
+ if ((this.motorType != Type.UNKNOWN) && (other.motorType != Type.UNKNOWN) &&
+ (this.motorType != other.motorType)) {
+ return false;
+ }
+
+ // Compare delays
+ if (this.delays.length != other.delays.length) {
+ return false;
+ }
for (int i=0; i < delays.length; i++) {
// INF - INF == NaN, which produces false when compared
if (Math.abs(this.delays[i] - other.delays[i]) > 0.5) {
return false;
}
}
+
return true;
}
} else {
- System.out.println("Falling back");
- System.out.println("o1:"+o1 + " o2:"+o2);
-
// Not understandable designation, simply compare strings
return COLLATOR.compare(o1, o2);
}
* if attempted.
*
* @param index the fin point index to remove
- * @throws IllegalFinPointException if removing the first or last fin point was attempted.
+ * @throws IllegalFinPointException if removing would result in invalid fin planform
*/
+ @SuppressWarnings("unchecked")
public void removePoint(int index) throws IllegalFinPointException {
if (index == 0 || index == points.size()-1) {
throw new IllegalFinPointException("cannot remove first or last point");
}
- // TODO: CRITICAL: Can result in invalid fin points
- points.remove(index);
+
+ ArrayList<Coordinate> copy = (ArrayList<Coordinate>) this.points.clone();
+ copy.remove(index);
+ validate(copy);
+ this.points = copy;
+
fireComponentChangeEvent(ComponentChangeEvent.BOTH_CHANGE);
}
return points.size();
}
- public void setPoints(Coordinate[] p) throws IllegalFinPointException {
- if (p[0].x != 0 || p[0].y != 0 || p[p.length-1].x < 0 || p[p.length-1].y != 0) {
- throw new IllegalFinPointException("Start or end point illegal.");
- }
- for (int i=0; i < p.length-1; i++) {
- for (int j=i+2; j < p.length-1; j++) {
- if (intersects(p[i].x, p[i].y, p[i+1].x, p[i+1].y,
- p[j].x, p[j].y, p[j+1].x, p[j+1].y)) {
- throw new IllegalFinPointException("segments intersect");
- }
- }
- if (p[i].z != 0) {
- throw new IllegalFinPointException("z-coordinate not zero");
- }
+ public void setPoints(Coordinate[] points) throws IllegalFinPointException {
+ ArrayList<Coordinate> list = new ArrayList<Coordinate>(points.length);
+ for (Coordinate p: points) {
+ list.add(p);
}
+ validate(list);
+ this.points = list;
- points.clear();
- for (Coordinate c: p) {
- points.add(c);
- }
- this.length = p[p.length-1].x;
+ this.length = points[points.length-1].x;
fireComponentChangeEvent(ComponentChangeEvent.BOTH_CHANGE);
}
((FreeformFinSet)c).points = (ArrayList<Coordinate>) this.points.clone();
return c;
}
+
+
+ private void validate(ArrayList<Coordinate> points) throws IllegalFinPointException {
+ final int n = points.size();
+ if (points.get(0).x != 0 || points.get(0).y != 0 ||
+ points.get(n-1).x < 0 || points.get(n-1).y != 0) {
+ throw new IllegalFinPointException("Start or end point illegal.");
+ }
+ for (int i=0; i < n-1; i++) {
+ for (int j=i+2; j < n-1; j++) {
+ if (intersects(points.get(i).x, points.get(i).y, points.get(i+1).x, points.get(i+1).y,
+ points.get(j).x, points.get(j).y, points.get(j+1).x, points.get(j+1).y)) {
+ throw new IllegalFinPointException("segments intersect");
+ }
+ }
+ if (points.get(i).z != 0) {
+ throw new IllegalFinPointException("z-coordinate not zero");
+ }
+ }
+ }
}
}
/**
- * NOTE: This value will also contain any possible acceleration peak when opening a parachute!
+ * NOTE: This value only takes into account flight phase.
*/
public double getMaxAcceleration() {
return maxAcceleration;
--- /dev/null
+package net.sf.openrocket.utils;
+
+import java.io.FileInputStream;
+import java.io.IOException;
+import java.util.ArrayList;
+import java.util.Arrays;
+import java.util.LinkedHashMap;
+import java.util.List;
+import java.util.Map;
+
+import net.sf.openrocket.file.GeneralMotorLoader;
+import net.sf.openrocket.motor.Motor;
+import net.sf.openrocket.util.Pair;
+
+public class GraphicalMotorSelector {
+
+ public static void main(String[] args) throws IOException {
+
+ if (args.length == 0) {
+ System.err.println("MotorPlot <files>");
+ System.exit(1);
+ }
+
+ // Load files
+ Map<String, List<Pair<String, Motor>>> map =
+ new LinkedHashMap<String, List<Pair<String, Motor>>>();
+
+ GeneralMotorLoader loader = new GeneralMotorLoader();
+ for (String file: args) {
+
+ for (Motor m: loader.load(new FileInputStream(file), file)) {
+ System.out.println("Loaded " + m + " from file "+file);
+
+ Pair<String, Motor> pair = new Pair<String, Motor>(file, m);
+ String key = m.getManufacturer() + ":" + m.getDesignation();
+
+ List<Pair<String, Motor>> list = map.get(key);
+ if (list == null) {
+ list = new ArrayList<Pair<String, Motor>>();
+ map.put(key, list);
+ }
+
+ list.add(pair);
+ }
+ }
+
+
+ // Go through different motors
+ int count = 0;
+ for (String key: map.keySet()) {
+ count++;
+ List<Pair<String, Motor>> list = map.get(key);
+
+
+ // Select best one of identical motors
+ List<String> filenames = new ArrayList<String>();
+ List<Motor> motors = new ArrayList<Motor>();
+ for (Pair<String, Motor> pair: list) {
+ String file = pair.getU();
+ Motor m = pair.getV();
+
+ int index = indexOf(motors, m);
+ if (index >= 0) {
+ // Replace previous if this has more delays, a known type or longer comment
+ Motor m2 = motors.get(index);
+ if (m.getStandardDelays().length > m2.getStandardDelays().length ||
+ (m2.getMotorType() == Motor.Type.UNKNOWN &&
+ m.getMotorType() != Motor.Type.UNKNOWN) ||
+ (m.getDescription().trim().length() >
+ m2.getDescription().trim().length())) {
+
+ filenames.set(index, file);
+ motors.set(index, m);
+
+ }
+ } else {
+ filenames.add(file);
+ motors.add(m);
+ }
+ }
+
+ if (filenames.size() == 0) {
+
+ System.out.println("ERROR selecting from " + list);
+ System.exit(1);
+
+ } else if (filenames.size() == 1) {
+
+ select(filenames.get(0), list, false);
+
+ } else {
+
+ System.out.println("Choosing from " + filenames +
+ " (" + count + "/" + map.size() + ")");
+ MotorPlot plot = new MotorPlot(filenames, motors);
+ plot.setVisible(true);
+ plot.dispose();
+ int n = plot.getSelected();
+ if (n < 0) {
+ System.out.println("NONE SELECTED from " + filenames);
+ } else {
+ select(filenames.get(n), list, true);
+ }
+
+ }
+
+ }
+
+ }
+
+ private static void select(String selected, List<Pair<String, Motor>> list, boolean manual) {
+ System.out.print("SELECT " + selected + " ");
+ if (manual) {
+ System.out.println("(manual)");
+ } else if (list.size() == 1) {
+ System.out.println("(only)");
+ } else {
+ System.out.println("(identical)");
+ }
+
+ boolean started = false;
+ for (Pair<String, Motor> pair: list) {
+ String file = pair.getU();
+ if (!file.equals(selected)) {
+ System.out.println("IGNORE " + file);
+ }
+ }
+ }
+
+
+ private static int indexOf(List<Motor> motors, Motor motor) {
+ for (int i=0; i<motors.size(); i++) {
+ Motor m = motors.get(i);
+ if (m.similar(motor)) {
+ if (m.getStandardDelays().length == 0 || motor.getStandardDelays().length == 0 ||
+ Arrays.equals(m.getStandardDelays(), motor.getStandardDelays())) {
+ return i;
+ }
+ }
+ }
+ return -1;
+ }
+}
package net.sf.openrocket.utils;
import java.awt.Color;
+import java.awt.event.ActionEvent;
+import java.awt.event.ActionListener;
import java.io.FileInputStream;
import java.io.IOException;
import java.util.ArrayList;
+import java.util.Arrays;
import java.util.List;
import javax.swing.BorderFactory;
+import javax.swing.JButton;
+import javax.swing.JDialog;
import javax.swing.JFrame;
import javax.swing.JPanel;
import javax.swing.JTabbedPane;
import org.jfree.data.xy.XYSeries;
import org.jfree.data.xy.XYSeriesCollection;
-public class MotorPlot extends JFrame {
+public class MotorPlot extends JDialog {
+ private int selected = -1;
public MotorPlot(List<String> filenames, List<Motor> motors) {
+ super((JFrame)null, "Motor plot", true);
JTabbedPane tabs = new JTabbedPane();
for (int i=0; i<filenames.size(); i++) {
JPanel pane = createPlotPanel((ThrustCurveMotor) motors.get(i));
+
+ JButton button = new JButton("Select");
+ final int number = i;
+ button.addActionListener(new ActionListener() {
+ @Override
+ public void actionPerformed(ActionEvent e) {
+ selected = number;
+ MotorPlot.this.setVisible(false);
+ }
+ });
+ pane.add(button, "wrap", 0);
+
tabs.addTab(filenames.get(i), pane);
}
JTextArea area = new JTextArea(5, 40);
StringBuilder sb = new StringBuilder();
sb.append("Designation: ").append(motor.getDesignation()).append(" ");
- sb.append("Manufacturer: ").append(motor.getManufacturer()).append('\n');
+ sb.append("Manufacturer: ").append(motor.getManufacturer()).append(" ");
+ sb.append("Type: ").append(motor.getMotorType()).append('\n');
+ sb.append("Delays: ").append(Arrays.toString(motor.getStandardDelays())).append('\n');
sb.append("Comment:\n").append(motor.getDescription());
area.setText(sb.toString());
- panel.add(area, "grow");
+ panel.add(area, "grow, wrap");
return panel;
}
+
+ public int getSelected() {
+ return selected;
+ }
+
+
public static void main(String[] args) throws IOException {
if (args.length == 0) {
System.err.println("MotorPlot <files>");
projects / debian / openrocket / commitdiff
