K1100T Data (RockSim)
Accuracy of this data file:
|
This File |
Certified |
± |
Diameter |
54 mm |
54 mm |
= |
Length |
410 mm |
398 mm |
+3% |
Prop. Weight |
791 g |
773 g |
+2% |
Total Weight |
1,426 g |
1,336 g |
+7% |
Avg. Thrust |
1,056.7 N |
1,100.0 N |
−4% |
Max. Thrust |
1,627.6 N |
2,004.0 N |
−19% |
Total Impulse |
1,618.9 Ns |
1,472.0 Ns |
+10% |
Burn Time |
1.5 s |
1.6 s |
−5% |
File Errors
File is usable, but has some problems:
- eng-data/t value "0" not after previous point
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Data Graph
File Notes
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Raw Data
<engine-database>
<engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="208.59" Itot="1618.86" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1011.78" burn-time="1.6" cgDiv="10" cgFix="1" cgStep="-1." code="K1100T" delays="6,10,14,18" dia="54." exitDia="0." initWt="1426.1" len="410." mDiv="10" mFix="1" mStep="-1." massFrac="55.49" mfg="Aerotech" peakThrust="1627.57" propWt="791.4" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<data>
<eng-data cg="205." f="0." m="791.4" t="0."/>
<eng-data cg="205." f="1627.57" m="791.4" t="0."/>
<eng-data cg="205." f="1244.55" m="721.196" t="0.1"/>
<eng-data cg="205." f="1196.65" m="542.184" t="0.4"/>
<eng-data cg="205." f="1124.9" m="315.2" t="0.8"/>
<eng-data cg="205." f="1077.04" m="207.555" t="1."/>
<eng-data cg="205." f="1053.06" m="155.488" t="1.1"/>
<eng-data cg="205." f="1029.09" m="104.594" t="1.2"/>
<eng-data cg="205." f="660.53" m="21.9947" t="1.4"/>
<eng-data cg="205." f="119.65" m="2.92463" t="1.5"/>
<eng-data cg="205." f="0." m="0." t="1.6"/>
</data>
</engine>
</engine-list>
</engine-database>
You can also download the raw data points as a CSV file.