G125T Data (RockSim)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
29 mm |
29 mm |
= |
| Length |
127 mm |
124 mm |
+2% |
| Prop. Weight |
62 g |
60 g |
+4% |
| Total Weight |
127 g |
125 g |
+2% |
| Avg. Thrust |
129.8 N |
125.0 N |
+4% |
| Max. Thrust |
155.2 N |
160.0 N |
−3% |
| Total Impulse |
124.8 Ns |
128.0 Ns |
−2% |
| Burn Time |
1.0 s |
1.0 s |
+1% |
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Raw Data
<engine-database>
<engine-list>
<engine mfg="Aerotech" code="G125T-14A" Type="single-use" dia="29." len="127."
initWt="127." propWt="62." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="124.681" peakThrust="155.17" throatDia="0." exitDia="0."
Itot="124.805" burn-time="1." massFrac="48.82" Isp="205.27" 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>At DMS G125</comments>
<data>
<eng-data t="0." f="0." m="62." cg="63.5"/>
<eng-data t="0.008" f="89.654" m="61.8218" cg="63.5"/>
<eng-data t="0.017" f="117.24" m="61.3593" cg="63.5"/>
<eng-data t="0.027" f="119.654" m="60.7709" cg="63.5"/>
<eng-data t="0.047" f="111.033" m="59.6249" cg="63.5"/>
<eng-data t="0.115" f="124.826" m="55.6412" cg="63.5"/>
<eng-data t="0.2" f="134.136" m="50.1738" cg="63.5"/>
<eng-data t="0.399" f="149.308" m="36.1634" cg="63.5"/>
<eng-data t="0.601" f="155.17" m="20.8865" cg="63.5"/>
<eng-data t="0.8" f="138.274" m="6.38183" cg="63.5"/>
<eng-data t="0.824" f="133.791" m="4.75997" cg="63.5"/>
<eng-data t="0.878" f="88.964" m="1.77218" cg="63.5"/>
<eng-data t="0.914" f="44.482" m="0.578913" cg="63.5"/>
<eng-data t="0.933" f="22.414" m="0.263207" cg="63.5"/>
<eng-data t="0.974" f="2.069" m="0.0138756" cg="63.5"/>
<eng-data t="1.001" f="0." m="0." cg="63.5"/>
</data>
</engine>
</engine-list>
</engine-database>
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