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

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m (*update to 0.24.2;)
m (*update to 0.25;)
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|tolerance=7
 
|tolerance=7
 
|research=Aerodynamics
 
|research=Aerodynamics
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|unlock cost=4000
 
|since=0.15
 
|since=0.15
|part=JetEngine
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|filename=jetEngineBasic.cfg
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|part=jetEngineBasic
 
|more=
 
|more=
 
{{Infobox/Part/JetEngine
 
{{Infobox/Part/JetEngine
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|isp=2000
 
|isp=2000
 
|vectoring=1.0
 
|vectoring=1.0
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}}
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{{Infobox/Part/test subject
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|environments=7
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|staging=True
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|event=True
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}}
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{{Infobox/Part/title|je}}
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{{Infobox/Part/jet engine
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|thrust=150
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|vectoring=1
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|isp=8
 
}}
 
}}
 
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Revision as of 00:43, 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) 1.000 t
Drag 0.2
Max. Temp. 3600 K
Impact Tolerance 7 m/s
Research Tech tree aerodynamics.png Aerodynamics
Unlock cost 4 000 Funds
Since version 0.15
Part configuration jetEngineBasic.cfg

Template:Infobox/Part/JetEngine

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
Jet engine
Maximum thrust 150.00 kN
Isp (max) 8 s
Fuel consumption 382.39 Units of fuel/s
Intake air consumption 0.00 Air unit/s
Thrust vectoring 1 °