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

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(fixed inaccurate stats, as of .23)
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{{Infobox/Part/JetEngine
+
<noinclude>{{Data template used}}</noinclude>{{Infobox/Part
|file=Basicjetengine.png
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|file=J33WheesleyBasicJetEngine.png
|size=s
+
|type=je
|costs=950
+
|size=1
|mass=1
+
|manufacturer=C7
 +
|costs=1400
 +
|mass=1.5
 
|drag=0.2
 
|drag=0.2
|temp=3600
+
|temp=2000
 
|tolerance=7
 
|tolerance=7
|fuel=0.0955
+
|research=Aerodynamics
|stall=15
+
|unlock cost=4000
|thrust=150
 
|opt-air=200
 
|in-size=1.1
 
|in-pow=125
 
|vectoring=1.0
 
 
|since=0.15
 
|since=0.15
|part=JetEngine
+
|filename=jetEngineBasic.cfg
|manufacturer=C7
+
|part=jetEngines
 +
|parent=Engine
 +
|more={{Infobox/Part/jet engine
 +
|thrust=120
 +
|isp=10500
 +
|intake=127
 +
}}
 +
{{Infobox/Part/generator
 +
|generate=4
 +
}}
 +
{{Infobox/Part/test subject
 +
|environments=15
 +
|event=y
 +
|staging=y
 +
}}
 +
{{Infobox/Part/cargo
 +
|volume=-1
 +
|stack=1
 +
}}
 
}}
 
}}

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