Difference between revisions of "J-90 "Goliath" Turbofan Engine/Box"
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Revision as of 22:11, 17 April 2018
J-90 "Goliath" Turbofan Engine | ||
Jet engine by C7 Aerospace Division | ||
Cost | (total) | 2 600.00 |
Mass | (total) | 4.50 t |
Drag | 0.2 | |
Max. Temp. | 2000 K | |
Volume | ? | |
Impact Tolerance | 7 m/s | |
Research | Heavy Aerodynamics | |
Unlock cost | 15 000 | |
Since version | 1.0.5 | |
Part configuration | jetEngineBig.cfg | |
Maximum thrust | 360 kN | |
Isp | (max) | 12600 s |
Fuel consumption | 0.58 /s | |
Intake air consumption | 0.00 /s | |
Thrust vectoring | No | |
Intake speed | 30 | |
Intake area | 0.03 m2 | |
Maximum intake air | 3.4 |