3 <engine mfg="Aerotech" code="H250G" Type="reloadable" dia="29." len="228.93"
\r
4 initWt="256." propWt="116.3" delays="0,6,10,14" auto-calc-mass="1"
\r
5 auto-calc-cg="1" avgThrust="251.105" peakThrust="320.655" throatDia="0."
\r
6 exitDia="0." Itot="231.017" burn-time="0.92" massFrac="0." Isp="0." 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
9 <comments>I don't know that
\r
11 delays are correct.
\r
14 test thrust curves.
\r
16 11/11/07.</comments>
\r
18 <eng-data t="0." f="0." m="0." cg="0."/>
\r
19 <eng-data t="0.00250627" f="88.6915" m="0." cg="0."/>
\r
20 <eng-data t="0.0125313" f="177.383" m="0." cg="0."/>
\r
21 <eng-data t="0.0300752" f="279.719" m="0." cg="0."/>
\r
22 <eng-data t="0.0726817" f="311.103" m="0." cg="0."/>
\r
23 <eng-data t="0.145363" f="320.654" m="0." cg="0."/>
\r
24 <eng-data t="0.24812" f="311.103" m="0." cg="0."/>
\r
25 <eng-data t="0.308271" f="297.458" m="0." cg="0."/>
\r
26 <eng-data t="0.398496" f="282.448" m="0." cg="0."/>
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27 <eng-data t="0.45614" f="270.168" m="0." cg="0."/>
\r
28 <eng-data t="0.593985" f="238.785" m="0." cg="0."/>
\r
29 <eng-data t="0.691729" f="221.047" m="0." cg="0."/>
\r
30 <eng-data t="0.799499" f="218.318" m="0." cg="0."/>
\r
31 <eng-data t="0.83208" f="210.131" m="0." cg="0."/>
\r
32 <eng-data t="0.844612" f="189.663" m="0." cg="0."/>
\r
33 <eng-data t="0.907268" f="13.6449" m="0." cg="0."/>
\r
34 <eng-data t="0.92" f="0." m="0." cg="0."/>
\r