version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / AeroTech_L1300.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="185.26" Itot="4556.42" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1301.84" burn-time="3.5" cgDiv="10" cgFix="1" cgStep="-1." code="L1300R" delays="1000" dia="98." exitDia="0." initWt="4884." len="443." mDiv="10" mFix="1" mStep="-1." massFrac="51.35" mfg="Aerotech" peakThrust="1552.47" propWt="2508." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4 <data>\r
5 <eng-data cg="221.5" f="0." m="2508." t="0."/>\r
6 <eng-data cg="221.5" f="1299.23" m="2499.71" t="0.0231839"/>\r
7 <eng-data cg="221.5" f="1332.26" m="2152.71" t="0.502318"/>\r
8 <eng-data cg="221.5" f="1497.42" m="1767.53" t="0.996909"/>\r
9 <eng-data cg="221.5" f="1552.47" m="1345.9" t="1.49923"/>\r
10 <eng-data cg="221.5" f="1508.43" m="929.249" t="1.99382"/>\r
11 <eng-data cg="221.5" f="1354.29" m="533.488" t="2.49614"/>\r
12 <eng-data cg="221.5" f="1101.05" m="194.053" t="2.99845"/>\r
13 <eng-data cg="221.5" f="1090.03" m="114.828" t="3.12983"/>\r
14 <eng-data cg="221.5" f="1145.09" m="62.5348" t="3.21484"/>\r
15 <eng-data cg="221.5" f="176.167" m="6.33201" t="3.3694"/>\r
16 <eng-data cg="221.5" f="0." m="0." t="3.5"/>\r
17 </data>\r
18 </engine>\r
19  </engine-list>\r
20 </engine-database>\r