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

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m (UmbralRaptor moved page J-33 "Wheesley" Basic Jet Engine/Box to J-33 "Wheesley" Turbofan Engine/Box: Engine was renamed.)
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|size=s
 
|size=s
 
|manufacturer=C7
 
|manufacturer=C7
|costs=950
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|costs=1400
 
|mass=1.5
 
|mass=1.5
 
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|filename=jetEngineBasic.cfg
 
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|more={{Infobox/Part/title|je}}
 
{{Infobox/Part/jet engine
 
{{Infobox/Part/jet engine
|isp=9600
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|intake=127 <!-- Amount of Air required per 1 unit of LF (Calc: Air / LF) -->
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|isp=10500
 
|thrust=120
 
|thrust=120
 
|vectoring=
 
|vectoring=
 
}}
 
}}
 
{{Infobox/Part/test subject
 
{{Infobox/Part/test subject
|environments=71
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|environments=15
 
|event=True
 
|event=True
 
|staging=True
 
|staging=True
 
}}
 
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Latest revision as of 11:25, 18 August 2018

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) 1.50 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
Jet engine
Maximum thrust 120 kN
Isp (max) 10500 s
Fuel consumption 0.23 Units of fuel/s
Intake air consumption 29.60 Air unit/s
Thrust vectoring × No
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