Difference between revisions of "O-10 "Puff" MonoPropellant Fuel Engine/Box"
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|file=O-10 MonoPropellant Engine.png | |file=O-10 MonoPropellant Engine.png | ||
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|size=r | |size=r | ||
|manufacturer=RS | |manufacturer=RS | ||
Revision as of 16:40, 14 April 2018
| 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 ° | |
| ||
