3 <engine mfg="Gorilla_Rocket_Motors" code="M1025WC" Type="reloadable" dia="98."
\r
4 len="869.95" initWt="10138." propWt="5329." delays="1000" auto-calc-mass="1"
\r
5 auto-calc-cg="1" avgThrust="1024.39" peakThrust="1780." throatDia="0."
\r
6 exitDia="0." Itot="9590.88" burn-time="9.36" massFrac="52.56" Isp="183.52"
\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="5329." cg="434.975"/>
\r
11 <eng-data t="0.1" f="1780." m="5279.55" cg="434.975"/>
\r
12 <eng-data t="0.5" f="1558." m="4908.61" cg="434.975"/>
\r
13 <eng-data t="3.25641" f="1500." m="2566.87" cg="434.975"/>
\r
14 <eng-data t="6.17949" f="795.082" m="703.085" cg="434.975"/>
\r
15 <eng-data t="9.3625" f="0." m="0." cg="434.975"/>
\r