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

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Line 8: Line 8:
 
|mass=4.5
 
|mass=4.5
 
|tolerance=7
 
|tolerance=7
|temp=2000 // = 3600
+
|temp=2000
 
|drag=0.2
 
|drag=0.2
 
|research=Heavy Aerodynamics
 
|research=Heavy Aerodynamics
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|isp=12600
 
|isp=12600
 
|thrust=360
 
|thrust=360
|vectoring=0
+
|vectoring=
 
}}
 
}}
 
{{Infobox/Part/air intake
 
{{Infobox/Part/air intake

Revision as of 05:22, 26 November 2015

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
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 0.00 Air unit/s
Thrust vectoring No
Intake speed 30
Intake area 0.03 m2
Maximum intake air 3.4 Air unit