version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / AeroTech_I132.rse
1 <engine-database>\r
2  <engine-list>\r
3 <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
4 <data>\r
5 <eng-data cg="165." f="0." m="324.4" t="0."/>\r
6 <eng-data cg="165." f="89." m="323.047" t="0.06"/>\r
7 <eng-data cg="165." f="227." m="207.716" t="1.5"/>\r
8 <eng-data cg="165." f="143." m="67.0506" t="3."/>\r
9 <eng-data cg="165." f="0." m="0." t="4.85"/>\r
10 </data>\r
11 </engine>\r
12  </engine-list>\r
13 </engine-database>\r