3 <engine FDiv="10" FFix="1" FStep="-1." Isp="172.24" Itot="3488.55" Type="unspecified" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1102.23" burn-time="3.17" cgDiv="10" cgFix="1" cgStep="-1." code="L1150" delays="1000" dia="75." exitDia="0." initWt="3673.6" len="531." mDiv="10" mFix="1" mStep="-1." massFrac="56.22" mfg="Aerotech" peakThrust="1309.71" propWt="2065.28" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
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4 <comments>AeroTech L1150
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5 provided by ThrustCurve.org (www.thrustcurve.org)
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8 <eng-data cg="265.5" f="0." m="2065.28" t="0."/>
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9 <eng-data cg="265.5" f="935.855" m="2050.6" t="0.053"/>
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10 <eng-data cg="265.5" f="1292.64" m="1970.12" t="0.175"/>
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14 <eng-data cg="265.5" f="1272.29" m="1597.01" t="0.675"/>
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15 <eng-data cg="265.5" f="1287.61" m="1502.29" t="0.8"/>
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16 <eng-data cg="265.5" f="1301.01" m="1406.51" t="0.925"/>
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17 <eng-data cg="265.5" f="1309.71" m="1311.45" t="1.048"/>
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18 <eng-data cg="265.5" f="1308.42" m="1216.9" t="1.17"/>
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19 <eng-data cg="265.5" f="1304.83" m="1120.21" t="1.295"/>
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20 <eng-data cg="265.5" f="1285.27" m="1024.37" t="1.42"/>
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21 <eng-data cg="265.5" f="1267.66" m="929.913" t="1.545"/>
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22 <eng-data cg="265.5" f="1255.62" m="836.549" t="1.67"/>
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23 <eng-data cg="265.5" f="1227.21" m="744.682" t="1.795"/>
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24 <eng-data cg="265.5" f="1202.44" m="654.783" t="1.92"/>
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25 <eng-data cg="265.5" f="1182.62" m="567.945" t="2.043"/>
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26 <eng-data cg="265.5" f="1150.71" m="483.681" t="2.165"/>
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28 <eng-data cg="265.5" f="1081.74" m="318.351" t="2.415"/>
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29 <eng-data cg="265.5" f="1037.55" m="239.935" t="2.54"/>
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30 <eng-data cg="265.5" f="1007.09" m="164.281" t="2.665"/>
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31 <eng-data cg="265.5" f="1008.91" m="89.6868" t="2.79"/>
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32 <eng-data cg="265.5" f="643.124" m="28.5598" t="2.915"/>
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33 <eng-data cg="265.5" f="64.371" m="2.38179" t="3.04"/>
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34 <eng-data cg="265.5" f="0." m="0." t="3.165"/>
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