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 Fund
Mass (total) 4.50 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 7 m/s
Research HeavyAerodynamics.png Heavy Aerodynamics
Unlock cost 15000 Fund
Since version 1.0.5
Part configuration jetEngines
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