3 <engine mfg="AT-RMS" code="I225FJ" Type="reloadable" dia="38." len="240." initWt="486."
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4 propWt="264." auto-calc-mass="1" auto-calc-cg="1" avgThrust="206.264"
\r
5 peakThrust="275.9" throatDia="0." exitDia="0." Itot="371.275" burn-time="1.8"
\r
6 massFrac="54.32" Isp="143.41" tDiv="10" tStep="-1." tFix="1" FDiv="10"
\r
7 FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
\r
9 <comments>Converted from RASP file by Chris Kobel mfr data
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10 Curvefit to instruction sheet on Aerotech website (12/27/06)</comments>
\r
12 <eng-data t="0." f="0." m="264." cg="120."/>
\r
13 <eng-data t="0.04" f="213.6" m="260.962" cg="120."/>
\r
14 <eng-data t="0.1" f="213.6" m="251.849" cg="120."/>
\r
15 <eng-data t="0.2" f="213.6" m="236.661" cg="120."/>
\r
16 <eng-data t="0.28" f="218.1" m="224.382" cg="120."/>
\r
17 <eng-data t="0.3" f="235.9" m="221.154" cg="120."/>
\r
18 <eng-data t="0.4" f="249.2" m="203.907" cg="120."/>
\r
19 <eng-data t="0.5" f="262.6" m="185.711" cg="120."/>
\r
20 <eng-data t="0.6" f="267." m="166.882" cg="120."/>
\r
21 <eng-data t="0.7" f="271.5" m="147.737" cg="120."/>
\r
22 <eng-data t="0.8" f="275.9" m="128.275" cg="120."/>
\r
23 <eng-data t="0.87" f="275.9" m="114.542" cg="120."/>
\r
24 <eng-data t="0.9" f="271.5" m="108.704" cg="120."/>
\r
25 <eng-data t="1." f="258.1" m="89.8748" cg="120."/>
\r
26 <eng-data t="1.1" f="240.3" m="72.1551" cg="120."/>
\r
27 <eng-data t="1.2" f="218.1" m="55.8576" cg="120."/>
\r
28 <eng-data t="1.3" f="200.3" m="40.9821" cg="120."/>
\r
29 <eng-data t="1.4" f="178." m="27.5324" cg="120."/>
\r
30 <eng-data t="1.5" f="160.2" m="15.5083" cg="120."/>
\r
31 <eng-data t="1.6" f="97.9" m="6.33202" cg="120."/>
\r
32 <eng-data t="1.7" f="40.1" m="1.42568" cg="120."/>
\r
33 <eng-data t="1.8" f="0." m="0." cg="120."/>
\r