3 <engine FDiv="10" FFix="1" FStep="-1." Isp="175.59" Itot="210.078" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="207.998" burn-time="1.01" cgDiv="10" cgFix="1" cgStep="-1." code="H210R" delays="10,1000" dia="29." exitDia="0." initWt="249." len="238." mDiv="10" mFix="1" mStep="-1." massFrac="49." mfg="Aerotech" peakThrust="260.22" propWt="122." tDiv="10" tFix="1" tStep="-1." throatDia="0.">
\r
5 <eng-data cg="119." f="0." m="122." t="0."/>
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6 <eng-data cg="119." f="105.92" m="121.385" t="0.02"/>
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7 <eng-data cg="119." f="211.29" m="117.701" t="0.06"/>
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8 <eng-data cg="119." f="219.77" m="112.694" t="0.1"/>
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9 <eng-data cg="119." f="229.64" m="107.474" t="0.14"/>
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10 <eng-data cg="119." f="235.08" m="102.077" t="0.18"/>
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11 <eng-data cg="119." f="241.59" m="96.5402" t="0.22"/>
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12 <eng-data cg="119." f="242.71" m="90.9152" t="0.26"/>
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13 <eng-data cg="119." f="245.35" m="85.2465" t="0.3"/>
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14 <eng-data cg="119." f="249.1" m="79.5036" t="0.34"/>
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15 <eng-data cg="119." f="253.41" m="73.6671" t="0.38"/>
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16 <eng-data cg="119." f="258.55" m="67.7208" t="0.42"/>
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17 <eng-data cg="119." f="260.22" m="61.6955" t="0.46"/>
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18 <eng-data cg="119." f="258." m="55.6765" t="0.5"/>
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19 <eng-data cg="119." f="259.25" m="49.6688" t="0.54"/>
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20 <eng-data cg="119." f="256.61" m="43.6772" t="0.58"/>
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21 <eng-data cg="119." f="252.44" m="37.7647" t="0.62"/>
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22 <eng-data cg="119." f="245.06" m="31.9864" t="0.66"/>
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23 <eng-data cg="119." f="219.91" m="26.5859" t="0.7"/>
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24 <eng-data cg="119." f="209.34" m="21.6003" t="0.74"/>
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25 <eng-data cg="119." f="200.59" m="16.8391" t="0.78"/>
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26 <eng-data cg="119." f="193.57" m="12.261" t="0.82"/>
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27 <eng-data cg="119." f="184.32" m="7.87196" t="0.86"/>
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28 <eng-data cg="119." f="153.88" m="2.96184" t="0.91"/>
\r
29 <eng-data cg="119." f="58.24" m="1.11405" t="0.94"/>
\r
30 <eng-data cg="119." f="13.21" m="0.0767152" t="0.99"/>
\r
31 <eng-data cg="119." f="0." m="0." t="1.01"/>
\r
projects / debian / openrocket / blob