|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:bore
|
120 mm
|
|
gptkbp:category
|
Junkers aircraft engines
V12 aircraft engines
|
|
gptkbp:compressionRatio
|
6.5:1 to 7.2:1 (varied by model)
|
|
gptkbp:configuration
|
V12
|
|
gptkbp:coolingSystem
|
liquid-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:Germany
|
|
gptkbp:displacement
|
19.7 L
|
|
gptkbp:engineType
|
liquid-cooled V12
|
|
gptkbp:firstFlight
|
1934
|
|
gptkbp:fuelType
|
aviation gasoline
direct fuel injection (in some variants)
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Junkers Jumo 210
|
|
gptkbp:manufacturer
|
gptkb:Junkers
|
|
gptkbp:notableFeature
|
first German production engine with direct fuel injection
|
|
gptkbp:numberOfEngines
|
12
|
|
gptkbp:powerOutput
|
610–700 hp
|
|
gptkbp:productionStartYear
|
1934–1938
|
|
gptkbp:stroke
|
140 mm
|
|
gptkbp:successor
|
gptkb:Junkers_Jumo_211
|
|
gptkbp:usedDuring
|
World War II (early years)
|
|
gptkbp:usedInAircraft
|
gptkb:Heinkel_He_112
gptkb:Arado_Ar_68
gptkb:Dornier_Do_17
gptkb:Messerschmitt_Bf_109
|
|
gptkbp:weight
|
510 kg (approximate dry weight)
|
|
gptkbp:bfsParent
|
gptkb:Ju_87A
|
|
gptkbp:bfsLayer
|
7
|