L952W Data (RockSim)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
98 mm |
98 mm |
= |
| Length |
443 mm |
427 mm |
+4% |
| Prop. Weight |
2,660 g |
2,750 g |
−3% |
| Total Weight |
5,027 g |
5,012 g |
= |
| Avg. Thrust |
776.5 N |
952.0 N |
−18% |
| Max. Thrust |
1,056.4 N |
1,021.5 N |
+3% |
| Total Impulse |
5,097.9 Ns |
4,656.0 Ns |
+9% |
| Burn Time |
6.6 s |
6.2 s |
+7% |
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="195.43" Itot="5097.92" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="760.884" burn-time="6.7" cgDiv="10" cgFix="1" cgStep="-1." code="L952W" delays="1000" dia="98." exitDia="0." initWt="5026.5" len="443." mDiv="10" mFix="1" mStep="-1." massFrac="52.92" mfg="Aerotech" peakThrust="1056.44" propWt="2660." tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<data>
<eng-data cg="221.5" f="0." m="2660." t="0."/>
<eng-data cg="221.5" f="1.51" m="2660." t="0."/>
<eng-data cg="221.5" f="776.75" m="2639.7" t="0.1"/>
<eng-data cg="221.5" f="909.97" m="2243.65" t="1."/>
<eng-data cg="221.5" f="962.28" m="2097.12" t="1.3"/>
<eng-data cg="221.5" f="1056.44" m="1307.12" t="2.8"/>
<eng-data cg="221.5" f="1047.59" m="1032.66" t="3.3"/>
<eng-data cg="221.5" f="1034.25" m="978.343" t="3.4"/>
<eng-data cg="221.5" f="887.78" m="677.479" t="4."/>
<eng-data cg="221.5" f="519.39" m="200.227" t="5.3"/>
<eng-data cg="221.5" f="288.5" m="52.6869" t="6."/>
<eng-data cg="221.5" f="0." m="0." t="6.7"/>
</data>
</engine>
</engine-list>
</engine-database>
You can also download the raw data points as a CSV file.
