J-90 "Goliath" Turbofan Engine/Box
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< J-90 "Goliath" Turbofan Engine
Revision as of 05:22, 26 November 2015 by VariousMetals (talk | contribs)
J-90 "Goliath" Turbofan Engine | ||
Jet engine by C7 Aerospace Division | ||
Cost | (total) | 2 600.00 |
Mass | (total) | 4.500 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 | |
Maximum thrust | 360.00 kN | |
Isp | (max) | 12600 s |
Fuel consumption | 0.58 /s | |
Intake air consumption | 0.00 /s | |
Thrust vectoring | No | |
Intake speed | 30 m/s | |
Intake area | 3 m2 |