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

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|file=J33WheesleyBasicJetEngine.png
 
|file=J33WheesleyBasicJetEngine.png
 
|type=je
 
|type=je
|size=s
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|size=1
 
|manufacturer=C7
 
|manufacturer=C7
 
|costs=1400
 
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|since=0.15
 
|since=0.15
 
|filename=jetEngineBasic.cfg
 
|filename=jetEngineBasic.cfg
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|part=jetEngines
|more={{Infobox/Part/title|je}}
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|parent=Engine
{{Infobox/Part/jet engine
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|more={{Infobox/Part/jet engine
|intake=127 <!-- Amount of Air required per 1 unit of LF (Calc: Air / LF) -->
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|thrust=120
|isp=10500
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|isp=10500
|thrust=120
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|intake=127
|vectoring=
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|generate=4
 
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{{Infobox/Part/test subject
 
{{Infobox/Part/test subject
|environments=15
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|environments=15
|event=True
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|event=y
|staging=True
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|staging=y
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}}
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{{Infobox/Part/cargo
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|volume=-1
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Latest revision as of 20:14, 9 October 2024

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) 1 400.00 Funds
Mass (total) 1.500 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.cfg
Maximum thrust 120.00 kN
Isp (max) 10500 s
Fuel consumption 0.23 Units of fuel/s
Intake air consumption 29.60 Air unit/s
Thrust vectoring No
Electricity generated 4 ⚡/s
Testing Environments
On the surface Yes
In the ocean Yes
On the launchpad Yes
In the atmosphere Yes
Sub-orbital No
In an orbit No
On an escape No
Docked No
Test by staging Yes
Manually testable Yes
Packed volume None