G104T Data (RockSim)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
29 mm |
29 mm |
= |
| Length |
125 mm |
125 mm |
= |
| Prop. Weight |
41 g |
44 g |
−7% |
| Total Weight |
136 g |
136 g |
= |
| Avg. Thrust |
93.1 N |
104.0 N |
−10% |
| Max. Thrust |
118.5 N |
113.8 N |
+4% |
| Total Impulse |
82.9 Ns |
81.5 Ns |
+2% |
| Burn Time |
0.9 s |
1.0 s |
−11% |
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="207.1" Itot="82.862" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="92.069" burn-time="0.9" cgDiv="10" cgFix="1" cgStep="-1." code="G104T" delays="6,10,14" dia="29." exitDia="0." initWt="135.6" len="125." mDiv="10" mFix="1" mStep="-1." massFrac="30.09" mfg="Aerotech" peakThrust="118.5" propWt="40.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<data>
<eng-data cg="62.5" f="0." m="40.8" t="0."/>
<eng-data cg="62.5" f="118.5" m="40.8" t="0."/>
<eng-data cg="62.5" f="114.14" m="35.0726" t="0.1"/>
<eng-data cg="62.5" f="114.14" m="29.4525" t="0.2"/>
<eng-data cg="62.5" f="109.91" m="23.9366" t="0.3"/>
<eng-data cg="62.5" f="109.91" m="18.5248" t="0.4"/>
<eng-data cg="62.5" f="105.68" m="13.2171" t="0.5"/>
<eng-data cg="62.5" f="84.56" m="8.53352" t="0.6"/>
<eng-data cg="62.5" f="71.83" m="4.68332" t="0.7"/>
<eng-data cg="62.5" f="59.2" m="1.45746" t="0.8"/>
<eng-data cg="62.5" f="0." m="0." t="0.9"/>
</data>
</engine>
</engine-list>
</engine-database>
You can also download the raw data points as a CSV file.
