O-10 "Puff" MonoPropellant Fuel Engine
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Revision as of 13:19, 15 July 2014 by XZise (talk | contribs) (Created page with "{{Future article|v=0.24}} {{:O-10 MonoPropellant Engine/Box}} The '''O-10 MonoPropellant Engine''' is the first stock reaction engine which does use monopropellant bu...")
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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The O-10 MonoPropellant Engine is the first stock reaction engine which does use monopropellant but works like a liquid fuel engine. So the engine is throttleable and doesn't react on the lateral movement commands for the normal RCS system. It does not show the fuel meter beside the staging icon.
The specific impulse is identical to the LV-1R Liquid Fuel Engine which can be placed radially too. Because monopropellant does not require plumbing to transfer the fuel from the tank to the engines, it is possible to place that engine on any part.
Changes
- 0.24 (projected)
- Initial release
References
- “Kerbal Space Program - Early Access Look At Update v0.24” by Scott Manley released on July 14, 2014