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= | ||
|size=r | |size=r | ||
|manufacturer=RS | |manufacturer=RS | ||
| − | |costs= | + | |costs=150 |
|mass=0.09 | |mass=0.09 | ||
|drag=0.2 | |drag=0.2 | ||
| + | |temp=2000 | ||
|tolerance=7 | |tolerance=7 | ||
| − | | | + | |research=Precision Propulsion |
| + | |unlock cost=2500 | ||
|since=0.24 | |since=0.24 | ||
| − | |part= | + | |physics insignificant=y |
| − | | | + | |filename=omsEngine.cfg |
| + | |part=OMSEngine | ||
| + | |parent=Engine | ||
|more={{Infobox/Part/reaction engine | |more={{Infobox/Part/reaction engine | ||
| − | |thrust=20 | + | |thrust=20 |
| − | |isp-atm= | + | |isp-atm=120 |
| − | |isp-vac= | + | |isp-vac=250 |
| − | |vectoring= | + | |vectoring=6 |
| − | |fuel=mp | + | |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 | |
| ||
