3 <engine mfg="Gorilla_Rocket_Motors" code="M1610BL" Type="reloadable" dia="75."
\r
4 len="1039." initWt="6918." propWt="3674." delays="1000" auto-calc-mass="1"
\r
5 auto-calc-cg="1" avgThrust="1613.68" peakThrust="2206.87" throatDia="0."
\r
6 exitDia="0." Itot="5986.77" burn-time="3.71" massFrac="53.11" Isp="166.16"
\r
7 tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
\r
8 mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
\r
10 <eng-data t="0." f="0." m="3674." cg="519.5"/>
\r
11 <eng-data t="0.0627746" f="1560.33" m="3643.95" cg="519.5"/>
\r
12 <eng-data t="1.3" f="2135.15" m="2241.02" cg="519.5"/>
\r
13 <eng-data t="1.64783" f="2206.87" m="1777.59" cg="519.5"/>
\r
14 <eng-data t="1.79535" f="2206.87" m="1577.8" cg="519.5"/>
\r
15 <eng-data t="1.89893" f="2189.63" m="1438.07" cg="519.5"/>
\r
16 <eng-data t="1.98996" f="2155.15" m="1316.72" cg="519.5"/>
\r
17 <eng-data t="2.50157" f="1715.5" m="709.085" cg="519.5"/>
\r
18 <eng-data t="2.82486" f="1474.12" m="392.677" cg="519.5"/>
\r
19 <eng-data t="2.99435" f="1241.36" m="251.452" cg="519.5"/>
\r
20 <eng-data t="3.29253" f="594.82" m="83.4515" cg="519.5"/>
\r
21 <eng-data t="3.5" f="355.858" m="22.9305" cg="519.5"/>
\r
22 <eng-data t="3.71" f="0." m="0." cg="519.5"/>
\r