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

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Revision as of 00:51, 8 October 2014

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-33 "Wheesley" Turbofan Engine
Part image
Jet engine by
C7 Aerospace Division

Radial size Small
Cost (total) 950.00 Funds
Mass (total) 1.00 t
Drag 0.2
Max. Temp. 3600 K
Volume  ?
Impact Tolerance 7 m/s
Research Tech tree aerodynamics.png Aerodynamics
Unlock cost 4 000 Funds
Since version 0.15
Part configuration jetEngineBasic.cfg
Maximum thrust 150 kN
Isp (max) 2000 s
Fuel consumption 1.53 Units of fuel/s
Intake air consumption 0.00 Air unit/s
Thrust vectoring 1 °
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 No
Docked No
Test by staging Yes
Manually testable Yes