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

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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) 4.500 t
Drag 0.2
Max. Temp. 2000 K
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 360.00 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 m/s
Intake area 3 m2
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