Difference between revisions of "RE-J10 "Wolfhound" Liquid Fuel Engine/Box"
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Latest revision as of 21:01, 21 September 2024
| RE-J10 "Wolfhound" Liquid Fuel Engine | ||
 | ||
| Liquid fuel engine by Rockomax Conglomerate | ||
| Radial size | Large | |
| Cost | (total) | 3 000.00 
|
| Mass | (total) | 3.300 t |
| Drag | 0.2 | |
| Max. Temp. | 2000 K | |
| Impact Tolerance | 6 m/s | |
| Research |  Very Heavy Rocketry
| |
| Unlock cost | 12 000
| |
| Since version | 1.4.1 | |
| Part configuration | LiquidEngineRE-J10.cfg | |
| Maximum thrust | (1 atm) | 69.08 kN |
| (vacuum) | 375.00 kN | |
| Isp | (1 atm) | 70 s |
| (vacuum) | 380 s | |
| Fuel consumption | 20.13  /s
| |
| Thrust vectoring | 3.0 ° | |
| Electricity generated | 8.0 ⚡/s | |
| Testing Environments | ||
| On the surface | Yes | |
| In the ocean | Yes | |
| On the launchpad | Yes | |
| In the atmosphere | Yes | |
| Sub-orbital | Yes | |
| In an orbit | Yes | |
| On an escape | Yes | |
| Docked | No | |
| Test by staging | Yes | |
| Manually testable | Yes | |
