Difference between revisions of "Kerbodyne KR-2L+ "Rhino" Liquid Fuel Engine/Box"
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Revision as of 14:18, 18 January 2017
| Kerbodyne KR-2L+ "Rhino" Liquid Fuel Engine | ||
 | ||
| Liquid fuel engine by Kerbodyne | ||
| Radial size | Extra large | |
| Cost | (total) | 25 000.00 
|
| Mass | (total) | 9.000 t |
| Drag | 0.2 | |
| Max. Temp. | 2000 K | |
| Impact Tolerance | 7 m/s | |
| Research |  Very Heavy Rocketry
| |
| Unlock cost | 68 000
| |
| Since version | 0.23.5 | |
| Part configuration | part.cfg | |
| Maximum thrust | (1 atm) | 1 205.88 kN |
| (vacuum) | 2 000.00 kN | |
| Isp | (1 atm) | 205 s |
| (vacuum) | 340 s | |
| Fuel consumption | 119.97  /s
| |
| Thrust vectoring | 4 ° | |
| Testing Environments | ||
| On the surface | Yes | |
| In the ocean | Yes | |
| On the launchpad | Yes | |
| In the atmosphere | Yes | |
| Sub-orbital | No | |
| In an orbit | No | |
| On an escape | No | |
| Docked | No | |
| Test by staging | Yes | |
| Manually testable | Yes | |
