version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / Contrail_G300.rse
1 <engine-database>\r
2  <engine-list>\r
3 <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
4 <comments>G-300 PVC Motor for 38mm/16 Inch Case.\r
5 Motor uses Fast Nozzle\r
6 90cc's of Nitrous Oxide Used\r
7 </comments>\r
8 <data>\r
9 <eng-data cg="203.2" f="0." m="23." t="0."/>\r
10 <eng-data cg="203.2" f="602.221" m="22.9234" t="0.00111857"/>\r
11 <eng-data cg="203.2" f="814.367" m="15.0852" t="0.0497763"/>\r
12 <eng-data cg="203.2" f="670.655" m="6.49069" t="0.100671"/>\r
13 <eng-data cg="203.2" f="266.893" m="5.05962" t="0.114094"/>\r
14 <eng-data cg="203.2" f="239.52" m="2.48301" t="0.158837"/>\r
15 <eng-data cg="203.2" f="0." m="0." t="0.25"/>\r
16 </data>\r
17 </engine>\r
18  </engine-list>\r
19 </engine-database>\r