version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / AeroTech_L952.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="195.43" Itot="5097.92" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="760.884" burn-time="6.7" cgDiv="10" cgFix="1" cgStep="-1." code="L952W" delays="1000" dia="98." exitDia="0." initWt="5026.5" len="443." mDiv="10" mFix="1" mStep="-1." massFrac="52.92" mfg="Aerotech" peakThrust="1056.44" propWt="2660." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4 <data>\r
5 <eng-data cg="221.5" f="0." m="2660." t="0."/>\r
6 <eng-data cg="221.5" f="1.51" m="2660." t="0."/>\r
7 <eng-data cg="221.5" f="776.75" m="2639.7" t="0.1"/>\r
8 <eng-data cg="221.5" f="909.97" m="2243.65" t="1."/>\r
9 <eng-data cg="221.5" f="962.28" m="2097.12" t="1.3"/>\r
10 <eng-data cg="221.5" f="1056.44" m="1307.12" t="2.8"/>\r
11 <eng-data cg="221.5" f="1047.59" m="1032.66" t="3.3"/>\r
12 <eng-data cg="221.5" f="1034.25" m="978.343" t="3.4"/>\r
13 <eng-data cg="221.5" f="887.78" m="677.479" t="4."/>\r
14 <eng-data cg="221.5" f="519.39" m="200.227" t="5.3"/>\r
15 <eng-data cg="221.5" f="288.5" m="52.6869" t="6."/>\r
16 <eng-data cg="221.5" f="0." m="0." t="6.7"/>\r
17 </data>\r
18 </engine>\r
19  </engine-list>\r
20 </engine-database>\r