version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / Contrail_H303.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="760.96" Itot="171.637" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="286.061" burn-time="0.6" cgDiv="10" cgFix="1" cgStep="-1." code="H303" delays="1000" dia="38." exitDia="0." initWt="589." len="508." mDiv="10" mFix="1" mStep="-1." massFrac="3.9" mfg="Contrail" peakThrust="780.15" propWt="23." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4 <comments>H-303-PVC Hybrid Motor\r
5 Uses Fast Nozzle\r
6 38mm/20 Inch Hardware\r
7 Uses 185cc Nitrous Oxide\r
8 </comments>\r
9 <data>\r
10 <eng-data cg="254." f="0." m="23." t="0."/>\r
11 <eng-data cg="254." f="663.812" m="23." t="0."/>\r
12 <eng-data cg="254." f="780.15" m="18.6712" t="0.0447427"/>\r
13 <eng-data cg="254." f="704.872" m="12.3273" t="0.108501"/>\r
14 <eng-data cg="254." f="342.171" m="12.0919" t="0.111857"/>\r
15 <eng-data cg="254." f="328.484" m="9.1766" t="0.176734"/>\r
16 <eng-data cg="254." f="307.954" m="8.31804" t="0.196868"/>\r
17 <eng-data cg="254." f="0." m="0." t="0.6"/>\r
18 </data>\r
19 </engine>\r
20  </engine-list>\r
21 </engine-database>\r