Difference between revisions of "J-90 "Goliath" Turbofan Engine/Box"

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m (Update, Add intake, Add test)
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{{Infobox/Part
 
{{Infobox/Part
 
|file=J-90 Goliath Turbofan Engine.png
 
|file=J-90 Goliath Turbofan Engine.png
|since=1.0.5
 
 
|type=je
 
|type=je
 +
|size=l
 +
|size2=r
 +
|manufacturer=C7
 
|costs=2600
 
|costs=2600
 
|mass=4.5
 
|mass=4.5
 +
|drag=0.2
 +
|temp=2000
 
|tolerance=7
 
|tolerance=7
|temp=2000
 
|drag=0.2
 
 
|research=Heavy Aerodynamics
 
|research=Heavy Aerodynamics
 
|unlock cost=15000
 
|unlock cost=15000
|manufacturer=C7
+
|since=1.0.5
 
|filename=jetEngineBig.cfg
 
|filename=jetEngineBig.cfg
 
|part=jetEngines
 
|part=jetEngines
 
|more=
 
|more=
 
{{Infobox/Part/jet engine
 
{{Infobox/Part/jet engine
 +
|intake=227
 
|isp=12600
 
|isp=12600
 
|thrust=360
 
|thrust=360
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|area=0.03
 
|area=0.03
 
|max=3.4
 
|max=3.4
 +
}}
 +
{{Infobox/Part/test subject
 +
|environments=15
 +
|event=True
 +
|staging=True
 
}}
 
}}
 
}}
 
}}

Revision as of 10:16, 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-90 "Goliath" Turbofan Engine
Part image
Jet engine by
C7 Aerospace Division

Radial size Large, Radial mounted
Cost (total) 2 600.00 Funds
Mass (total) 4.50 t
Drag 0.2
Max. Temp. 2000 K
Volume  ?
Impact Tolerance 7 m/s
Research HeavyAerodynamics.png Heavy Aerodynamics
Unlock cost 15 000 Funds
Since version 1.0.5
Part configuration jetEngineBig.cfg
Maximum thrust 360 kN
Isp (max) 12600 s
Fuel consumption 0.58 Units of fuel/s
Intake air consumption 132.27 Air unit/s
Thrust vectoring No
Intake speed 30
Intake area 0.03 m2
Maximum intake air 3.4 Air unit
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