39 lines
1.7 KiB
Plaintext
39 lines
1.7 KiB
Plaintext
<engine-database>
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<engine-list>
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<engine mfg="Aerotech" code="H250G" Type="reloadable" dia="29." len="228.93"
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initWt="256." propWt="116.3" delays="0,6,10,14" auto-calc-mass="1"
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auto-calc-cg="1" avgThrust="251.105" peakThrust="320.655" throatDia="0."
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exitDia="0." Itot="231.017" burn-time="0.92" massFrac="0." Isp="0." tDiv="10"
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tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
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mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
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<comments>I don't know that
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these ejection
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delays are correct.
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This was made
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using the Aerotech
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test thrust curves.
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By Tobin Yehle,
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11/11/07.</comments>
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<data>
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<eng-data t="0." f="0." m="0." cg="0."/>
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<eng-data t="0.00250627" f="88.6915" m="0." cg="0."/>
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<eng-data t="0.0125313" f="177.383" m="0." cg="0."/>
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<eng-data t="0.0300752" f="279.719" m="0." cg="0."/>
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<eng-data t="0.0726817" f="311.103" m="0." cg="0."/>
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<eng-data t="0.145363" f="320.654" m="0." cg="0."/>
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<eng-data t="0.24812" f="311.103" m="0." cg="0."/>
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<eng-data t="0.308271" f="297.458" m="0." cg="0."/>
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<eng-data t="0.398496" f="282.448" m="0." cg="0."/>
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<eng-data t="0.45614" f="270.168" m="0." cg="0."/>
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<eng-data t="0.593985" f="238.785" m="0." cg="0."/>
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<eng-data t="0.691729" f="221.047" m="0." cg="0."/>
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<eng-data t="0.799499" f="218.318" m="0." cg="0."/>
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<eng-data t="0.83208" f="210.131" m="0." cg="0."/>
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<eng-data t="0.844612" f="189.663" m="0." cg="0."/>
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<eng-data t="0.907268" f="13.6449" m="0." cg="0."/>
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<eng-data t="0.92" f="0." m="0." cg="0."/>
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</data>
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</engine>
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</engine-list>
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</engine-database>
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