F52C Data (RockSim)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
29 mm |
29 mm |
= |
| Length |
111 mm |
111 mm |
= |
| Prop. Weight |
30 g |
30 g |
= |
| Total Weight |
81 g |
81 g |
= |
| Avg. Thrust |
52.8 N |
52.7 N |
= |
| Max. Thrust |
61.3 N |
64.3 N |
−5% |
| Total Impulse |
66.3 Ns |
66.2 Ns |
= |
| Burn Time |
1.3 s |
1.3 s |
= |
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Raw Data
<engine-database>
<engine-list>
<engine mfg="Aerotech" code="F52C" Type="single-use" dia="29." len="111." initWt="81.4"
propWt="30." delays="5,8,12" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="49.895" peakThrust="61.323" throatDia="0." exitDia="0." Itot="66.311"
burn-time="1.33" massFrac="36.86" Isp="225.39" 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 F52C, data from TMT test firing</comments>
<data>
<eng-data t="0." f="0." m="30." cg="55.5"/>
<eng-data t="0.02" f="0.267" m="29.9988" cg="55.5"/>
<eng-data t="0.024" f="3.465" m="29.9954" cg="55.5"/>
<eng-data t="0.038" f="38.82" m="29.8615" cg="55.5"/>
<eng-data t="0.073" f="53.881" m="29.1276" cg="55.5"/>
<eng-data t="0.143" f="56.492" m="27.3799" cg="55.5"/>
<eng-data t="0.323" f="61.323" m="22.5827" cg="55.5"/>
<eng-data t="0.826" f="57.346" m="9.08031" cg="55.5"/>
<eng-data t="1.141" f="51.074" m="1.3548" cg="55.5"/>
<eng-data t="1.17" f="35.612" m="0.786142" cg="55.5"/>
<eng-data t="1.225" f="11.761" m="0.196755" cg="55.5"/>
<eng-data t="1.266" f="4.559" m="0.0453946" cg="55.5"/>
<eng-data t="1.291" f="1.512" m="0.011062" cg="55.5"/>
<eng-data t="1.32" f="0.133" m="0.00027077" cg="55.5"/>
<eng-data t="1.329" f="0." m="0." cg="55.5"/>
</data>
</engine>
</engine-list>
</engine-database>
You can also download the raw data points as a CSV file.
