3 <engine FDiv="10" FFix="1" FStep="-1." Isp="134.05" Itot="32.865" Type="unspecified" auto-calc-cg="1" auto-calc-mass="1" avgThrust="11.613" burn-time="2.83" cgDiv="10" cgFix="1" cgStep="-1." code="E11J" delays="4" dia="24." exitDia="0." initWt="62.4" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="40.06" mfg="Aerotech" peakThrust="19.259" propWt="25." tDiv="10" tFix="1" tStep="-1." throatDia="0.">
\r
4 <comments>Based On NAR Test Data
\r
8 <eng-data cg="35." f="0." m="25." t="0."/>
\r
9 <eng-data cg="35." f="14.3704" m="24.6035" t="0.0725446"/>
\r
10 <eng-data cg="35." f="17.6296" m="23.5168" t="0.16183"/>
\r
11 <eng-data cg="35." f="18.3704" m="22.9055" t="0.206473"/>
\r
12 <eng-data cg="35." f="19.2593" m="19.8705" t="0.418527"/>
\r
13 <eng-data cg="35." f="18.3704" m="15.3979" t="0.731027"/>
\r
14 <eng-data cg="35." f="14.2222" m="8.13432" t="1.31696"/>
\r
15 <eng-data cg="35." f="9.03704" m="2.80264" t="1.91964"/>
\r
16 <eng-data cg="35." f="2.22222" m="0.269489" t="2.51116"/>
\r
17 <eng-data cg="35." f="0." m="0." t="2.83"/>
\r