Difference between revisions of "R121 Turboshaft Engine/Box"

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|mass=0.6
 
|mass=0.6
 
|ia=3
 
|ia=3
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|motorOutput=150
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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=150
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  |motorOutput=150
|motorCost=2
 
|motorMass=0.004
 
 
  |efficiency=0.4
 
  |efficiency=0.4
 
  |lf=0.01
 
  |lf=0.01
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}}
 
}}
 
{{Infobox/Part/cargo
 
{{Infobox/Part/cargo
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|volume=-1
 
  |stack=1
 
  |stack=1
|volume=-1
 
 
}}
 
}}
 
{{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).
R121 Turboshaft Engine
Part image
Turboshaft engine by
C7 Aerospace Division

Radial size Tiny
Cost (total) 500.00 Funds
(dry) 200.00 Funds
Mass (total) 1.215 t
(dry) 0.615 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 12 m/s
Research Tech tree aerodynamics.png Aerodynamics
Unlock cost 1 200 Funds
Since version 1.7.3
Part configuration RotorEngine_02.cfg
Fuel consumption 0.4 Units of fuel/s
Intake air consumption 18.8 Air unit/s
Intake speed 75 m/s
Intake area 0.5 m2
Electricity generated 0.4 ⚡/s
Packed volume None
Intake air 3 Air unit