Difference between revisions of "J-33 "Wheesley" Turbofan Engine/Box"

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m (UmbralRaptor moved page J-33 "Wheesley" Basic Jet Engine/Box to J-33 "Wheesley" Turbofan Engine/Box: Engine was renamed.)
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Revision as of 17:38, 17 January 2016

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J-33 "Wheesley" Turbofan Engine
Part image
Jet engine by
C7 Aerospace Division
Radial size Small
Cost (total) 950.00 Funds
Mass (total) 1.50 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 7 m/s
Research Tech tree aerodynamics.png Aerodynamics
Unlock cost 4 000 Funds
Since version 0.15
Part configuration jetEngineBasic
Maximum thrust 120 kN
Isp (max) 9600 s
Fuel consumption 0.25 Units of fuel/s
Intake air consumption 0.00 Air unit/s
Thrust vectoring × No
Testing Environments
On the surface ✓ Yes
In the ocean ✓ Yes
On the launchpad ✓ Yes
In the atmosphere × No
Sub orbital × No
In an orbit × No
On an escape ✓ Yes
Docked × No
Test by staging ✓ Yes
Manually testable ✓ Yes