Difference between revisions of "O-10 "Puff" MonoPropellant Fuel Engine/Box"
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|more={{Infobox/Part/reaction engine | |more={{Infobox/Part/reaction engine | ||
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Revision as of 23:11, 20 July 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 |
| Drag | 0.2 | |
| 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 | |
