HP-H135W Data (RockSim)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
29 mm |
29 mm |
= |
| Length |
216 mm |
216 mm |
= |
| Prop. Weight |
82 g |
82 g |
= |
| Total Weight |
212 g |
212 g |
= |
| Avg. Thrust |
116.1 N |
115.9 N |
= |
| Max. Thrust |
159.8 N |
159.9 N |
= |
| Total Impulse |
229.0 Ns |
225.8 Ns |
+1% |
| Burn Time |
2.0 s |
2.0 s |
+1% |
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Raw Data
<engine-database>
<engine-list>
<engine mfg="Aerotech" code="H135W" Type="single-use" dia="29." len="216." initWt="212."
propWt="82." delays="6,8,10,12,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="110.537" peakThrust="159.806" throatDia="0." exitDia="0."
Itot="229.032" burn-time="2.07" massFrac="38.68" Isp="284.81" 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>AeroTech Pro-SU 29mm H135 14sec adjustable delay.
From Tripoli Data Sheet updated 2013/02/10
Created by Robert Belknap 2013/03/04
</comments>
<data>
<eng-data t="0." f="0." m="82." cg="108."/>
<eng-data t="0.014" f="159.806" m="81.5995" cg="108."/>
<eng-data t="0.045" f="110.931" m="80.0971" cg="108."/>
<eng-data t="0.104" f="144.43" m="77.4" cg="108."/>
<eng-data t="0.131" f="135.643" m="76.0463" cg="108."/>
<eng-data t="0.252" f="154.315" m="69.7656" cg="108."/>
<eng-data t="0.293" f="130.701" m="67.6737" cg="108."/>
<eng-data t="0.387" f="149.921" m="62.9515" cg="108."/>
<eng-data t="1.005" f="140.037" m="30.8732" cg="108."/>
<eng-data t="1.261" f="119.168" m="18.9944" cg="108."/>
<eng-data t="1.297" f="142.233" m="17.3098" cg="108."/>
<eng-data t="1.324" f="109.833" m="16.0915" cg="108."/>
<eng-data t="1.387" f="120.267" m="13.4964" cg="108."/>
<eng-data t="1.518" f="110.382" m="8.08751" cg="108."/>
<eng-data t="1.595" f="80.727" m="5.45324" cg="108."/>
<eng-data t="1.685" f="60.408" m="3.17938" cg="108."/>
<eng-data t="1.797" f="33.499" m="1.29658" cg="108."/>
<eng-data t="1.896" f="14.278" m="0.449851" cg="108."/>
<eng-data t="2.072" f="0." m="0." cg="108."/>
</data>
</engine>
</engine-list>
</engine-database>
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