J-90 "Goliath" Turbofan Engine/Box

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J-90 "Goliath" Turbofan Engine
Part image
Jet engine by
C7 Aerospace Division

Radial size Radial mounted
Cost (total) 2 600.00 Funds
Mass (total) 4.50 t
Drag 0.2
Max. Temp. 2000 K
Volume  ?
Impact Tolerance 7 m/s
Research HeavyAerodynamics.png Heavy Aerodynamics
Unlock cost 15 000 Funds
Since version 1.0.5
Part configuration jetEngineBig.cfg
Jet engine
Maximum thrust 360 kN
Isp (max) 12600 s
Fuel consumption 0.58 Units of fuel/s
Intake air consumption 132.27 Air unit/s
Thrust vectoring No
Intake speed 30
Intake area 0.03 m2
Maximum intake air 3.4 Air unit
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