openrocket/datafiles/thrustcurves/Cesaroni_M1520.rse

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<engine-database>
<engine-list>
<engine mfg="CTI" code="M1520-BS" Type="unspecified" dia="98." len="548." initWt="6718."
propWt="3737." delays="0" auto-calc-mass="1" auto-calc-cg="1" avgThrust="1547.7"
peakThrust="1827.11" throatDia="0." exitDia="0." Itot="7579.08" burn-time="4.9"
massFrac="55.63" Isp="206.81" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>Pro98-3G 7579M1520-BS P</comments>
<data>
<eng-data t="0." f="0." m="3737." cg="274."/>
<eng-data t="0.04" f="1427.8" m="3722.92" cg="274."/>
<eng-data t="0.082" f="1706.39" m="3690.47" cg="274."/>
<eng-data t="0.176" f="1620.49" m="3613.37" cg="274."/>
<eng-data t="0.748" f="1734.25" m="3140.29" cg="274."/>
<eng-data t="1.652" f="1827.11" m="2346.58" cg="274."/>
<eng-data t="2.676" f="1715.68" m="1452.21" cg="274."/>
<eng-data t="3.89" f="1423.15" m="512.779" cg="274."/>
<eng-data t="4.399" f="1404.58" m="157.939" cg="274."/>
<eng-data t="4.616" f="661.661" m="47.3998" cg="274."/>
<eng-data t="4.877" f="69.649" m="0.343417" cg="274."/>
<eng-data t="4.897" f="0." m="0." cg="274."/>
</data>
</engine>
</engine-list>
</engine-database>