version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / Contrail_I250.rse
1 <engine-database>\r
2  <engine-list>\r
3 <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
4 <comments>I-250-HP\r
5 38mm/28 Inch Hardware\r
6 430cc\r
7 Medium Nozzle\r
8 </comments>\r
9 <data>\r
10 <eng-data cg="355.6" f="0." m="66." t="0."/>\r
11 <eng-data cg="355.6" f="622.751" m="65.7868" t="0.00447427"/>\r
12 <eng-data cg="355.6" f="437.979" m="64.1525" t="0.0246085"/>\r
13 <eng-data cg="355.6" f="273.737" m="10.7884" t="1.00447"/>\r
14 <eng-data cg="355.6" f="171.085" m="10.1792" t="1.02237"/>\r
15 <eng-data cg="355.6" f="157.399" m="5.68061" t="1.20134"/>\r
16 <eng-data cg="355.6" f="136.868" m="4.82427" t="1.23937"/>\r
17 <eng-data cg="355.6" f="0." m="0." t="1.7"/>\r
18 </data>\r
19 </engine>\r
20  </engine-list>\r
21 </engine-database>\r