J-90 "Goliath" Turbofan Engine/Box
From Kerbal Space Program Wiki
| J-90 "Goliath" Turbofan Engine | ||
 | ||
| Jet engine by C7 Aerospace Division | ||
| Radial size | Radial mounted | |
| Cost | (total) | 2 600.00 
|
| (dry) | 2 600.00
| |
| Mass | (total) | 4.517 t |
| (dry) | 4.517 t | |
| Drag | 0.2 | |
| Max. Temp. | 2000 K | |
| Impact Tolerance | 7 m/s | |
| Research |  Heavy Aerodynamics
| |
| Unlock cost | 15 000
| |
| Since version | 1.0.5 | |
| Part configuration | jetEngineBig.cfg | |
| Intake speed | 30 m/s | |
| Intake area | 3 m2 | |
| Maximum thrust | 360.00 kN | |
| Isp | (max) | 12600 s |
| Fuel consumption | 0.58  /s
| |
| Intake air consumption | 132.27  /s
| |
| Thrust vectoring | No | |
| Electricity generated | 16 ⚡/s | |
| 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 | |
| Intake air | 3
| |
