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

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{{Infobox/Part/jet engine
{{Infobox/Part/jet engine
{{Infobox/Part/test subject
{{Infobox/Part/test subject

Revision as of 01:28, 19 December 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
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 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