Difference between revisions of "O-10 "Puff" MonoPropellant Fuel Engine/Box"
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|mass=0.09 | |mass=0.09 | ||
|drag=0.2 | |drag=0.2 | ||
+ | |temp=3600 | ||
|tolerance=7 | |tolerance=7 | ||
− | | | + | |research=Specialized Control |
|since=0.24 | |since=0.24 | ||
|part=OMSEngine | |part=OMSEngine | ||
− | | | + | |physics insignificant=y |
|more={{Infobox/Part/reaction engine | |more={{Infobox/Part/reaction engine | ||
|thrust=20 | |thrust=20 |
Revision as of 21:53, 11 August 2014
O-10 "Puff" MonoPropellant Fuel Engine | ||
Liquid fuel engine by Reaction Systems Ltd | ||
Radial size | Radial mounted | |
Cost | (total) | 800.00 |
Mass | (total) | 0.090 t [1] |
Drag | 0.2 [1] | |
Max. Temp. | 3600 K | |
Impact Tolerance | 7 m/s | |
Research | Specialized Control | |
Unlock cost | 0 | |
Since version | 0.24 | |
Part configuration | [[Parts/OMSEngine/{{{filename}}}|{{{filename}}}]] | |
Maximum thrust | (1 atm) | 15.17 kN |
(vacuum) | 20.00 kN | |
Isp | (1 atm) | 220 s |
(vacuum) | 290 s | |
Fuel consumption | 1.76 /s | |
Thrust vectoring | No | |
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