Simulator Data

Statistics	Declared	Calculated	Official
Motor:	AeroTech F52
Contributor:	John Coker
Submitted:	Feb 21, 2008
Last Updated:	Jun 25, 2008
Data Format:	RockSim
Data Source:	User-Created
License:	Unknown
Diameter (mm):	29.0		29.0
Length (cm):	12.4		12.4
Prop. Weight (g):	36.6		36.6
Total Weight (g):	121.4		—
Avg. Thrust (N):	51.4	53.7	51.4
Max. Thrust (N):	79.0	79.0	79.0
Tot. Impulse (Ns):	73.0	73.0	73.0
Burn Time (s):	1.4	1.4	1.4
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Data Graph

Alternates: in Pounds large size

Data File

<engine-database>
 <engine-list>
<engine FDiv="10" FFix="1" FStep="-1." Isp="203.25" Itot="72.95" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="51.374" burn-time="1.42" cgDiv="10" cgFix="1" cgStep="-1." code="F52" delays="5,8,11" dia="29." exitDia="0." initWt="121.4" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="30.15" mfg="Aerotech" peakThrust="78.95" propWt="36.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<comments>Aerotech F52 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data cg="62." f="0." m="36.6" t="0."/>
<eng-data cg="62." f="46.899" m="36.4588" t="0.012"/>
<eng-data cg="62." f="61.778" m="35.8863" t="0.033"/>
<eng-data cg="62." f="69.441" m="35.1292" t="0.056"/>
<eng-data cg="62." f="73.483" m="33.6592" t="0.097"/>
<eng-data cg="62." f="76.636" m="32.9814" t="0.115"/>
<eng-data cg="62." f="74.381" m="32.4131" t="0.13"/>
<eng-data cg="62." f="74.82" m="31.5523" t="0.153"/>
<eng-data cg="62." f="78.422" m="30.9757" t="0.168"/>
<eng-data cg="62." f="78.95" m="30.423" t="0.182"/>
<eng-data cg="62." f="77.963" m="29.4783" t="0.206"/>
<eng-data cg="62." f="77.504" m="28.2303" t="0.238"/>
<eng-data cg="62." f="73.892" m="27.4707" t="0.258"/>
<eng-data cg="62." f="72.974" m="25.4076" t="0.314"/>
<eng-data cg="62." f="72.046" m="22.6428" t="0.39"/>
<eng-data cg="62." f="70.679" m="21.2822" t="0.428"/>
<eng-data cg="62." f="65.699" m="18.7848" t="0.501"/>
<eng-data cg="62." f="62.975" m="16.719" t="0.565"/>
<eng-data cg="62." f="58.874" m="12.9593" t="0.688"/>
<eng-data cg="62." f="56.15" m="11.1992" t="0.749"/>
<eng-data cg="62." f="52.517" m="8.80035" t="0.837"/>
<eng-data cg="62." f="49.793" m="7.15779" t="0.901"/>
<eng-data cg="62." f="46.161" m="5.47285" t="0.971"/>
<eng-data cg="62." f="39.365" m="2.96266" t="1.088"/>
<eng-data cg="62." f="34.386" m="1.92661" t="1.144"/>
<eng-data cg="62." f="29.417" m="1.46246" t="1.173"/>
<eng-data cg="62." f="20.376" m="0.850406" t="1.222"/>
<eng-data cg="62." f="13.151" m="0.404654" t="1.275"/>
<eng-data cg="62." f="5.461" m="0.105843" t="1.339"/>
<eng-data cg="62." f="1.838" m="0.0142932" t="1.389"/>
<eng-data cg="62." f="0." m="0." t="1.42"/>
</data>
</engine>
 </engine-list>
</engine-database>

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