L1170FJ Data (RockSim)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
75 mm |
75 mm |
= |
| Length |
665 mm |
665 mm |
= |
| Prop. Weight |
2,800 g |
2,800 g |
= |
| Total Weight |
4,990 g |
4,990 g |
= |
| Avg. Thrust |
1,208.9 N |
1,141.0 N |
+6% |
| Max. Thrust |
1,473.3 N |
1,489.0 N |
−1% |
| Total Impulse |
4,214.5 Ns |
4,232.0 Ns |
= |
| Burn Time |
3.5 s |
3.7 s |
−6% |
Add this file to my outbox.
Data Graph
File Notes
Do you have a comment on this file?
Please add a note.
Raw Data
<engine-database>
<engine-list>
<engine mfg="Aerotech" code="L1170FJ" Type="reloadable" dia="75." len="665."
initWt="4990." propWt="2800." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1148.35" peakThrust="1473.29" throatDia="0." exitDia="0."
Itot="4214.45" burn-time="3.67" massFrac="56.11" Isp="153.48" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="2800." cg="332.5"/>
<eng-data t="0.031" f="992.64" m="2789.78" cg="332.5"/>
<eng-data t="0.072" f="1400.14" m="2757.19" cg="332.5"/>
<eng-data t="0.113" f="1473.29" m="2718.05" cg="332.5"/>
<eng-data t="0.144" f="1389.7" m="2688.57" cg="332.5"/>
<eng-data t="0.351" f="1285.21" m="2504.63" cg="332.5"/>
<eng-data t="1.495" f="1431.49" m="1472.22" cg="332.5"/>
<eng-data t="1.856" f="1431.49" m="1128.89" cg="332.5"/>
<eng-data t="2.227" f="1358.35" m="785.061" cg="332.5"/>
<eng-data t="2.753" f="1201.62" m="337.753" cg="332.5"/>
<eng-data t="2.928" f="1170.27" m="199.867" cg="332.5"/>
<eng-data t="3." f="1065.78" m="146.386" cg="332.5"/>
<eng-data t="3.113" f="679.175" m="80.8849" cg="332.5"/>
<eng-data t="3.247" f="355.261" m="34.8385" cg="332.5"/>
<eng-data t="3.361" f="177.63" m="14.6581" cg="332.5"/>
<eng-data t="3.464" f="83.591" m="5.72023" cg="332.5"/>
<eng-data t="3.67" f="0." m="0." cg="332.5"/>
</data>
</engine>
</engine-list>
</engine-database>
You can also download the raw data points as a CSV file.
