3 <engine mfg="Gorilla_Rocket_Motors" code="J485WC" Type="reloadable" dia="54." len="326."
\r
4 initWt="1164.8" propWt="549." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
\r
5 avgThrust="492.077" peakThrust="573.821" throatDia="0." exitDia="0."
\r
6 Itot="1077.65" burn-time="2.19" massFrac="47.13" Isp="200.16" tDiv="10"
\r
7 tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
\r
8 mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
\r
10 <eng-data t="0." f="0." m="549." cg="163."/>
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11 <eng-data t="0.05" f="263.913" m="545.639" cg="163."/>
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12 <eng-data t="0.095" f="401.808" m="538.008" cg="163."/>
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13 <eng-data t="0.15" f="444.822" m="526.147" cg="163."/>
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14 <eng-data t="0.503226" f="544.253" m="437.156" cg="163."/>
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15 <eng-data t="0.8" f="573.821" m="352.635" cg="163."/>
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16 <eng-data t="1.075" f="569.372" m="272.557" cg="163."/>
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17 <eng-data t="1.5" f="542.683" m="152.169" cg="163."/>
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18 <eng-data t="2." f="444.822" m="26.4002" cg="163."/>
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19 <eng-data t="2.1" f="311.376" m="7.13827" cg="163."/>
\r
20 <eng-data t="2.19" f="0." m="0." cg="163."/>
\r