HP-I65W Data (RockSim)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
54 mm |
54 mm |
= |
| Length |
218 mm |
218 mm |
= |
| Prop. Weight |
377 g |
377 g |
= |
| Total Weight |
752 g |
752 g |
= |
| Avg. Thrust |
87.5 N |
80.2 N |
+9% |
| Max. Thrust |
196.3 N |
145.0 N |
+35% |
| Total Impulse |
660.2 Ns |
635.0 Ns |
+4% |
| Burn Time |
7.5 s |
7.9 s |
−5% |
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Raw Data
<engine-database>
<engine-list>
<engine mfg="Aerotech" code="I65" Type="single-use" dia="54." len="218." initWt="752."
propWt="377." delays="10" auto-calc-mass="1" auto-calc-cg="1" avgThrust="77.709"
peakThrust="196.341" throatDia="0." exitDia="0." Itot="660.214" burn-time="8.5"
massFrac="50.13" Isp="178.58" 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="377." cg="109."/>
<eng-data t="0.023" f="148.274" m="376.026" cg="109."/>
<eng-data t="0.211" f="196.341" m="357.529" cg="109."/>
<eng-data t="0.398" f="167.827" m="338.085" cg="109."/>
<eng-data t="0.797" f="149.903" m="301.889" cg="109."/>
<eng-data t="1.395" f="135.239" m="253.205" cg="109."/>
<eng-data t="2.238" f="122.204" m="191.242" cg="109."/>
<eng-data t="3.199" f="99.392" m="130.441" cg="109."/>
<eng-data t="4.711" f="69.249" m="57.6389" cg="109."/>
<eng-data t="5.367" f="48.882" m="35.5133" cg="109."/>
<eng-data t="6.246" f="29.329" m="15.885" cg="109."/>
<eng-data t="6.926" f="15.479" m="7.18554" cg="109."/>
<eng-data t="7.395" f="11.406" m="3.58548" cg="109."/>
<eng-data t="8.496" f="0." m="0." cg="109."/>
</data>
</engine>
</engine-list>
</engine-database>
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