HP-I205W Data (RockSim)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
29 mm |
29 mm |
= |
| Length |
305 mm |
305 mm |
= |
| Prop. Weight |
188 g |
188 g |
= |
| Total Weight |
315 g |
315 g |
= |
| Avg. Thrust |
205.6 N |
205.0 N |
= |
| Max. Thrust |
377.3 N |
253.0 N |
+49% |
| Total Impulse |
346.4 Ns |
345.0 Ns |
= |
| Burn Time |
1.7 s |
1.7 s |
−1% |
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Raw Data
<engine-database>
<engine-list>
<engine mfg="Aerotech" code="I205" Type="single-use" dia="29." len="304.8" initWt="315."
propWt="188." delays="14" auto-calc-mass="1" auto-calc-cg="1" avgThrust="183.103"
peakThrust="377.299" throatDia="0." exitDia="0." Itot="346.431" burn-time="1.89"
massFrac="59.68" Isp="187.9" 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>From AT DMS announcement May 2014.</comments>
<data>
<eng-data t="0." f="0." m="188." cg="152.4"/>
<eng-data t="0.008" f="377.299" m="187.181" cg="152.4"/>
<eng-data t="0.028" f="241.932" m="183.821" cg="152.4"/>
<eng-data t="0.36" f="256.333" m="138.935" cg="152.4"/>
<eng-data t="0.711" f="246.252" m="91.0686" cg="152.4"/>
<eng-data t="0.861" f="233.292" m="71.5508" cg="152.4"/>
<eng-data t="1.121" f="230.411" m="38.8375" cg="152.4"/>
<eng-data t="1.146" f="214.571" m="35.819" cg="152.4"/>
<eng-data t="1.242" f="211.69" m="24.7155" cg="152.4"/>
<eng-data t="1.349" f="141.127" m="14.4721" cg="152.4"/>
<eng-data t="1.404" f="125.286" m="10.4963" cg="152.4"/>
<eng-data t="1.489" f="72.004" m="5.94604" cg="152.4"/>
<eng-data t="1.602" f="41.762" m="2.45783" cg="152.4"/>
<eng-data t="1.712" f="11.521" m="0.867484" cg="152.4"/>
<eng-data t="1.787" f="12.961" m="0.369266" cg="152.4"/>
<eng-data t="1.892" f="0." m="0." cg="152.4"/>
</data>
</engine>
</engine-list>
</engine-database>
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