Difference between revisions of "J-90 "Goliath" Turbofan Engine/Box"

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Revision as of 18:22, 20 November 2015

This is a data template. To add content which doesn't belong to this template edit the English page (or one of its translations).
J-90 "Goliath" Turbofan Engine
Part image
Jet engine by
C7 Aerospace Division
Cost (total) 2 600.00 Funds
Mass (total) 4.50 t
Drag 0.2
Max. Temp. 2000 // = 3600 K
Impact Tolerance 7 m/s
Research HeavyAerodynamics.png Heavy Aerodynamics
Unlock cost 15 000 Funds
Since version 1.0.5
Part configuration jetEngines
Maximum thrust 360 kN
Isp (max) 12600 s
Fuel consumption 0.58 Units of fuel/s
Intake air consumption 0.00 Air unit/s
Thrust vectoring 0 °
Intake speed 30
Intake area 0.03 m2
Maximum intake air 3.4 Air unit