Difference between revisions of "R7000 Turboshaft Engine/Box"

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|mass=1.2
 
|mass=1.2
 
|ia=3
 
|ia=3
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|motorOutput=550
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|motorCost=2
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|motorMass=0.004
 
|drag=0.2
 
|drag=0.2
 
|temp=2000
 
|temp=2000
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|part=Robotics
 
|part=Robotics
 
|more={{Infobox/Part/servo
 
|more={{Infobox/Part/servo
  |base=0.1
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  |baseRate=0.1
  |motor=550
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  |motorOutput=550
|motorCost=2
 
|motorMass=0.004
 
 
  |efficiency=0.4
 
  |efficiency=0.4
 
  |lf=0.012
 
  |lf=0.012
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}}
 
}}
 
{{Infobox/Part/tank
 
{{Infobox/Part/tank
|ia=3
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|ia=3
 
}}
 
}}
 
}}
 
}}

Latest revision as of 20:36, 21 September 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).
R7000 Turboshaft Engine
Part image
Turboshaft engine by
C7 Aerospace Division

Radial size Tiny
Cost (total) 1 650.00 Funds
(dry) 550.00 Funds
Mass (total) 3.415 t
(dry) 1.215 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 12 m/s
Research Advanced aerodynamics.png Advanced Aerodynamics
Unlock cost 5 000 Funds
Since version 1.7.3
Part configuration RotorEngine_03.cfg
Fuel consumption 1.7 Units of fuel/s
Intake air consumption 82.5 Air unit/s
Intake speed 75 m/s
Intake area 2 m2
Electricity generated 0.48 ⚡/s
Intake air 3 Air unit