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Wikidata

(Q564413)

English

Jumo 210

V-12 piston aircraft engine family by Junkers

  • Jumo 210 D
  • Jumo 210 G
  • Jumo 210D
  • Jumo 210C
  • Junkers Jumo 210
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Statements

instance of
engine model
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has use
aircraft engine
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image
Jumo-210.jpg
525 × 383; 52 KB
media legend
Vue du moteur. (French)
1 reference
imported from Wikimedia project
English Wikipedia
mass
442 kilogram
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start time
1932
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end time
1938
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manufacturer
Junkers
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engine configuration
V12
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inverted V engine
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coolant
liquid
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ethylene glycol
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fuel system
carburetor
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nominal power output
508 kilowatt
elevation above sea level
0 metre
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515 kilowatt
elevation above sea level
1,500 metre
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501 kilowatt
elevation above sea level
3,700 metre
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number of cylinders
12
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compression ratio
6.5
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bore
124 millimetre
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stroke
136 millimetre
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total produced
6,500
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length
1,478 millimetre
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width
686 millimetre
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height
960 millimetre
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source of energy
gasoline
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engine displacement
19,708.49 cubic centimetre
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Commons category
Junkers Jumo 210
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Identifiers

 
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