M1025WC Data (RockSim)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
98 mm |
98 mm |
= |
| Length |
870 mm |
870 mm |
= |
| Prop. Weight |
5,329 g |
5,329 g |
= |
| Total Weight |
10,138 g |
10,138 g |
= |
| Avg. Thrust |
1,065.5 N |
1,025.0 N |
+4% |
| Max. Thrust |
1,780.0 N |
1,852.0 N |
−4% |
| Total Impulse |
9,590.9 Ns |
9,580.0 Ns |
= |
| Burn Time |
9.0 s |
9.4 s |
−4% |
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Raw Data
<engine-database>
<engine-list>
<engine mfg="Gorilla_Rocket_Motors" code="M1025WC" Type="reloadable" dia="98."
len="869.95" initWt="10138." propWt="5329." delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="1024.39" peakThrust="1780." throatDia="0."
exitDia="0." Itot="9590.88" burn-time="9.36" massFrac="52.56" Isp="183.52"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="5329." cg="434.975"/>
<eng-data t="0.1" f="1780." m="5279.55" cg="434.975"/>
<eng-data t="0.5" f="1558." m="4908.61" cg="434.975"/>
<eng-data t="3.25641" f="1500." m="2566.87" cg="434.975"/>
<eng-data t="6.17949" f="795.082" m="703.085" cg="434.975"/>
<eng-data t="9.3625" f="0." m="0." cg="434.975"/>
</data>
</engine>
</engine-list>
</engine-database>
You can also download the raw data points as a CSV file.
