636I216-14A Data (RockSim)
Accuracy of this data file:
|
This File |
Certified |
± |
Diameter |
38 mm |
38 mm |
= |
Length |
367 mm |
367 mm |
= |
Prop. Weight |
313 g |
313 g |
= |
Total Weight |
601 g |
601 g |
= |
Avg. Thrust |
217.6 N |
216.1 N |
+1% |
Max. Thrust |
345.0 N |
379.5 N |
−9% |
Total Impulse |
636.1 Ns |
636.1 Ns |
= |
Burn Time |
2.9 s |
2.9 s |
−1% |
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Raw Data
<engine-database>
<engine-list>
<engine mfg="CTI" code="I216-CL(I)" Type="reloadable" dia="38." len="367." initWt="601."
propWt="312.5" delays="5,7,9,11,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="205.198" peakThrust="345." throatDia="0." exitDia="0." Itot="636.114"
burn-time="3.1" massFrac="52." Isp="207.57" 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>This motor is a standard Pro38-5G with a different nozzle to keep total impulse in 'I' range</comments>
<data>
<eng-data t="0." f="0." m="312.5" cg="183.5"/>
<eng-data t="0.017" f="35." m="312.354" cg="183.5"/>
<eng-data t="0.03" f="300." m="311.284" cg="183.5"/>
<eng-data t="0.035" f="345." m="310.492" cg="183.5"/>
<eng-data t="0.05" f="325." m="308.023" cg="183.5"/>
<eng-data t="0.07" f="275." m="305.076" cg="183.5"/>
<eng-data t="0.14" f="292." m="295.327" cg="183.5"/>
<eng-data t="0.26" f="296." m="277.995" cg="183.5"/>
<eng-data t="0.8" f="280." m="201.593" cg="183.5"/>
<eng-data t="1.1" f="280.4" m="160.298" cg="183.5"/>
<eng-data t="1.62" f="255." m="91.9118" cg="183.5"/>
<eng-data t="1.8" f="226." m="70.645" cg="183.5"/>
<eng-data t="2.105" f="210." m="37.9809" cg="183.5"/>
<eng-data t="2.2" f="195." m="28.5302" cg="183.5"/>
<eng-data t="2.45" f="80." m="11.643" cg="183.5"/>
<eng-data t="2.75" f="36." m="3.09496" cg="183.5"/>
<eng-data t="3.1" f="0." m="0." cg="183.5"/>
</data>
</engine>
</engine-list>
</engine-database>
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