37 lines
2.0 KiB
Plaintext
37 lines
2.0 KiB
Plaintext
<engine-database>
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<engine-list>
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<engine FDiv="10" FFix="1" FStep="-1." Isp="183.39" Itot="38.667" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="6.381" burn-time="6.06" cgDiv="10" cgFix="1" cgStep="-1." code="E6" delays="2,4,6,8,100" dia="24." exitDia="0." initWt="46.3" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="46.44" mfg="Apogee" peakThrust="20.12" propWt="21.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
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<comments>Aerotech E6 RASP.ENG file made from NAR published data
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File produced July 4, 2000
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The total impulse, peak thrust, average thrust and burn time are
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the same as the averaged static test data on the NAR web site in
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the certification file. The curve drawn with these data points is as
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close to the certification curve as can be with such a limited
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number of points (32) allowed with wRASP up to v1.6.
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</comments>
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<data>
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<eng-data cg="35." f="0." m="21.5" t="0."/>
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<eng-data cg="35." f="18.59" m="21.2106" t="0.056"/>
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<eng-data cg="35." f="20.12" m="20.6079" t="0.112"/>
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<eng-data cg="35." f="17.575" m="20.021" t="0.168"/>
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<eng-data cg="35." f="14.38" m="18.7862" t="0.307"/>
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<eng-data cg="35." f="10.45" m="17.2399" t="0.531"/>
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<eng-data cg="35." f="7.696" m="15.4086" t="0.894"/>
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<eng-data cg="35." f="6.244" m="14.432" t="1.146"/>
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<eng-data cg="35." f="5.808" m="12.6059" t="1.691"/>
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<eng-data cg="35." f="5.663" m="8.95436" t="2.836"/>
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<eng-data cg="35." f="5.517" m="5.65345" t="3.898"/>
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<eng-data cg="35." f="5.227" m="4.52736" t="4.275"/>
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<eng-data cg="35." f="4.937" m="4.13176" t="4.415"/>
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<eng-data cg="35." f="5.082" m="2.34073" t="5.058"/>
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<eng-data cg="35." f="5.227" m="1.01948" t="5.519"/>
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<eng-data cg="35." f="6.679" m="0.741439" t="5.603"/>
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<eng-data cg="35." f="3.921" m="0.370124" t="5.729"/>
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<eng-data cg="35." f="2.323" m="0.104528" t="5.882"/>
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<eng-data cg="35." f="1.016" m="0.0265515" t="5.966"/>
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<eng-data cg="35." f="0." m="-0." t="6.06"/>
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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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