3 <engine mfg="Cesaroni Technology Inc." code="L610" Type="reloadable" dia="98."
\r
4 len="427." initWt="4840." propWt="2415." delays="1000" auto-calc-mass="1"
\r
5 auto-calc-cg="1" avgThrust="595.595" peakThrust="929.678" throatDia="0."
\r
6 exitDia="0." Itot="4842.19" burn-time="8.13" massFrac="49.9" Isp="204.46"
\r
7 tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
\r
8 mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
\r
9 <comments>Data Entered by Tim Van Milligan based on RMS case weight.
\r
10 Based on CAR certification data
\r
11 This data has not been approved by Cesaroni or Canadian Association of Rocketry.
\r
14 <eng-data t="0." f="0." m="2415." cg="213.5"/>
\r
15 <eng-data t="0.155" f="929.678" m="2379.07" cg="213.5"/>
\r
16 <eng-data t="0.247" f="913.867" m="2336.77" cg="213.5"/>
\r
17 <eng-data t="0.355" f="891.846" m="2288.14" cg="213.5"/>
\r
18 <eng-data t="0.433" f="880.836" m="2253.66" cg="213.5"/>
\r
19 <eng-data t="0.618" f="897.352" m="2171.62" cg="213.5"/>
\r
20 <eng-data t="1.005" f="913.867" m="1996.83" cg="213.5"/>
\r
21 <eng-data t="1.87" f="902.857" m="1604.95" cg="213.5"/>
\r
22 <eng-data t="2.179" f="880.836" m="1467.51" cg="213.5"/>
\r
23 <eng-data t="2.411" f="875.331" m="1365.91" cg="213.5"/>
\r
24 <eng-data t="3.044" f="809.268" m="1099.99" cg="213.5"/>
\r
25 <eng-data t="3.988" f="677.143" m="750.081" cg="213.5"/>
\r
26 <eng-data t="4.853" f="550.523" m="485.267" cg="213.5"/>
\r
27 <eng-data t="5.502" f="500.975" m="315.091" cg="213.5"/>
\r
28 <eng-data t="5.889" f="473.449" m="221.052" cg="213.5"/>
\r
29 <eng-data t="6.306" f="456.934" m="124.304" cg="213.5"/>
\r
30 <eng-data t="6.507" f="401.881" m="81.2573" cg="213.5"/>
\r
31 <eng-data t="6.94" f="110.105" m="25.9743" cg="213.5"/>
\r
32 <eng-data t="7.172" f="66.063" m="15.7823" cg="213.5"/>
\r
33 <eng-data t="8.13" f="0." m="0." cg="213.5"/>
\r
projects / debian / openrocket / blob