I357T Data (RockSim)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
38 mm |
38 mm |
= |
| Length |
202 mm |
203 mm |
= |
| Prop. Weight |
166 g |
174 g |
−5% |
| Total Weight |
364 g |
343 g |
+6% |
| Avg. Thrust |
320.9 N |
357.0 N |
−10% |
| Max. Thrust |
465.5 N |
432.8 N |
+8% |
| Total Impulse |
341.0 Ns |
342.0 Ns |
= |
| Burn Time |
1.1 s |
1.0 s |
+6% |
File Errors
File is usable, but has some problems:
- eng-data/t value "0" not after previous point
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 FDiv="10" FFix="1" FStep="-1." Isp="209.22" Itot="341." Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="310." burn-time="1.1" cgDiv="10" cgFix="1" cgStep="-1." code="I357T" delays="6,10,14" dia="38." exitDia="0." initWt="363.5" len="202." mDiv="10" mFix="1" mStep="-1." massFrac="45.72" mfg="Aerotech" peakThrust="465.53" propWt="166.2" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
<data>
<eng-data cg="101." f="0." m="166.2" t="0."/>
<eng-data cg="101." f="465.53" m="166.2" t="0."/>
<eng-data cg="101." f="407.97" m="144.913" t="0.1"/>
<eng-data cg="101." f="394.67" m="86.2334" t="0.4"/>
<eng-data cg="101." f="363.62" m="49.2751" t="0.6"/>
<eng-data cg="101." f="319.23" m="32.6344" t="0.7"/>
<eng-data cg="101." f="257.18" m="18.5876" t="0.8"/>
<eng-data cg="101." f="190.69" m="7.67322" t="0.9"/>
<eng-data cg="101." f="62.09" m="1.5131" t="1."/>
<eng-data cg="101." f="0." m="0." t="1.1"/>
</data>
</engine>
</engine-list>
</engine-database>
You can also download the raw data points as a CSV file.
