version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / Contrail_H222.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="744.73" Itot="160.673" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="229.532" burn-time="0.7" cgDiv="10" cgFix="1" cgStep="-1." code="H222" delays="1000" dia="38." exitDia="0." initWt="520." len="406.4" mDiv="10" mFix="1" mStep="-1." massFrac="4.23" mfg="Contrail" peakThrust="684.342" propWt="22." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4 <comments>H-222-HP Reload\r
5 38mm/16 inch Case Used\r
6 Medium Nozzle Used For Reload\r
7 140cc of Nitrous Oxide Used\r
8 </comments>\r
9 <data>\r
10 <eng-data cg="203.2" f="0." m="22." t="0."/>\r
11 <eng-data cg="203.2" f="684.342" m="22." t="0."/>\r
12 <eng-data cg="203.2" f="656.968" m="19.2266" t="0.0302013"/>\r
13 <eng-data cg="203.2" f="574.847" m="17.34" t="0.0525727"/>\r
14 <eng-data cg="203.2" f="349.014" m="16.9863" t="0.0581655"/>\r
15 <eng-data cg="203.2" f="260.05" m="4.95265" t="0.346756"/>\r
16 <eng-data cg="203.2" f="191.616" m="4.39924" t="0.364653"/>\r
17 <eng-data cg="203.2" f="0." m="0." t="0.7"/>\r
18 </data>\r
19 </engine>\r
20  </engine-list>\r
21 </engine-database>\r