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

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Revision as of 13:41, 21 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-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 Aviation.png Aviation
Unlock cost 4 000 Funds
Since version 0.15
Part configuration jetEngineBasic
Maximum thrust 80 kN
Isp (max) 9600 s
Fuel consumption 0.17 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 ✓ Yes
Docked × No
Test by staging ✓ Yes
Manually testable ✓ Yes