|
gptkbp:instanceOf
|
gptkb:piston_engine
|
|
gptkbp:bore
|
135 mm
|
|
gptkbp:cancellationDate
|
technical difficulties
production problems
|
|
gptkbp:configuration
|
liquid-cooled
24-cylinder
|
|
gptkbp:coolingSystem
|
liquid-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:Germany
|
|
gptkbp:developedBy
|
1937-1944
|
|
gptkbp:diameter
|
1.18 m
|
|
gptkbp:displacement
|
46.4 L
|
|
gptkbp:engineType
|
gptkb:piston_engine
|
|
gptkbp:firstFlight
|
1939
|
|
gptkbp:fuelType
|
aviation gasoline
|
|
gptkbp:intendedUse
|
gptkb:Bomber_B_program
|
|
gptkbp:length
|
2.34 m
|
|
gptkbp:manufacturer
|
gptkb:Junkers
|
|
gptkbp:notableFeature
|
compact design
high power-to-weight ratio
|
|
gptkbp:numberOfEngines
|
24
six banks of four cylinders
|
|
gptkbp:powerOutput
|
2000-2500 hp
|
|
gptkbp:predecessor
|
gptkb:Junkers_Jumo_211
|
|
gptkbp:projectCancelled
|
1944
|
|
gptkbp:status
|
experimental
not mass produced
|
|
gptkbp:stroke
|
135 mm
|
|
gptkbp:successor
|
none
|
|
gptkbp:supercharger
|
single-stage
|
|
gptkbp:usedInAircraft
|
gptkb:Junkers_Ju_290
gptkb:Junkers_Ju_388
gptkb:Dornier_Do_317
gptkb:Junkers_Ju_288
|
|
gptkbp:weight
|
approx. 1,350 kg
|
|
gptkbp:bfsParent
|
gptkb:Junkers_Jumo_213
gptkb:X_Engine
|
|
gptkbp:bfsLayer
|
8
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Junkers Jumo 222
|