Difference between revisions of "O-10 "Puff" MonoPropellant Fuel Engine/Box"
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− | <noinclude>{{Data template used}}</noinclude> | + | <noinclude>{{Data template used}}</noinclude>{{Infobox/Part |
− | {{Infobox/Part | + | |file=O-10.png |
− | |file=O-10 | ||
|type=mpe | |type=mpe | ||
|size=r | |size=r | ||
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|unlock cost=2500 | |unlock cost=2500 | ||
|since=0.24 | |since=0.24 | ||
+ | |physics insignificant=y | ||
|filename=omsEngine.cfg | |filename=omsEngine.cfg | ||
|part=OMSEngine | |part=OMSEngine | ||
− | | | + | |parent=Engine |
|more={{Infobox/Part/reaction engine | |more={{Infobox/Part/reaction engine | ||
− | | | + | |thrust=20 |
− | |isp-atm=120 | + | |isp-atm=120 |
− | |isp-vac=250 | + | |isp-vac=250 |
− | | | + | |vectoring=6 |
− | | | + | |fuel=mp |
+ | }} | ||
+ | {{Infobox/Part/cargo | ||
+ | |volume=260 | ||
}} | }} | ||
}} | }} |
Latest revision as of 20:24, 9 October 2024
O-10 "Puff" MonoPropellant Fuel Engine | ||
Monopropellant engine by Reaction Systems Ltd | ||
Radial size | Radial mounted | |
Cost | (total) | 150.00 |
Mass | (total) | 0.090 t [1] |
Drag | 0.2 [1] | |
Max. Temp. | 2000 K | |
Impact Tolerance | 7 m/s | |
Research | Precision Propulsion | |
Unlock cost | 2 500 | |
Since version | 0.24 | |
Part configuration | omsEngine.cfg | |
Maximum thrust | (1 atm) | 9.60 kN |
(vacuum) | 20.00 kN | |
Isp | (1 atm) | 120 s |
(vacuum) | 250 s | |
Fuel consumption | 2.04 /s | |
Thrust vectoring | 6 ° | |
Packed volume | 260 l | |
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