Difference between revisions of "J-90 "Goliath" Turbofan Engine/Box"
From Kerbal Space Program Wiki
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| + | |more={{Infobox/Part/air intake | ||
| + | |speed=30 | ||
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| − | |isp=12600 | + | |isp=12600 |
| − | | | + | |intake=227 |
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{{Infobox/Part/test subject | {{Infobox/Part/test subject | ||
| − | |environments=15 | + | |environments=15 |
| − | |event= | + | |event=y |
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| + | }} | ||
| + | {{Infobox/Part/tank | ||
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Latest revision as of 20:16, 9 October 2024
| 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
| |
