]> git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/Cesaroni_N1100.rse
b6e0c3a2503d8efc377fc03bd13677d11322812f
[debian/openrocket] / datafiles / thrustcurves / Cesaroni_N1100.rse
1 <engine-database>\r
2   <engine-list>\r
3 <engine  mfg="Cesaroni Technology Inc." code="N1100" Type="reloadable" dia="98."\r
4 len="1046." initWt="11589." propWt="4728." delays="1000" auto-calc-mass="1"\r
5 auto-calc-cg="1" avgThrust="1121.14" peakThrust="2708.97" throatDia="0."\r
6 exitDia="0." Itot="14003." burn-time="12.49" massFrac="40.8" Isp="302.01"\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>N1100 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
12 </comments>\r
13 <data>\r
14 <eng-data  t="0." f="0." m="4728." cg="523."/>\r
15 <eng-data  t="0.16" f="2624." m="4657.12" cg="523."/>\r
16 <eng-data  t="0.33" f="2708.97" m="4504.07" cg="523."/>\r
17 <eng-data  t="0.835" f="2025.92" m="4100.4" cg="523."/>\r
18 <eng-data  t="1.22" f="1886." m="3846.14" cg="523."/>\r
19 <eng-data  t="1.6" f="1734.81" m="3613.86" cg="523."/>\r
20 <eng-data  t="2.44" f="1713." m="3124.93" cg="523."/>\r
21 <eng-data  t="2.75" f="1823.77" m="2939.83" cg="523."/>\r
22 <eng-data  t="3.184" f="1783.69" m="2675.52" cg="523."/>\r
23 <eng-data  t="4.2" f="1601.36" m="2094.91" cg="523."/>\r
24 <eng-data  t="5.6" f="1312.23" m="1406.28" cg="523."/>\r
25 <eng-data  t="7." f="978.609" m="864.847" cg="523."/>\r
26 <eng-data  t="9.8" f="427.029" m="200.404" cg="523."/>\r
27 <eng-data  t="12.025" f="88.0836" m="6.91471" cg="523."/>\r
28 <eng-data  t="12.49" f="0." m="0." cg="523."/>\r
29 </data>\r
30 </engine>\r
31 </engine-list>\r
32 </engine-database>\r