|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:bore
|
135 mm
|
|
gptkbp:cancellationDate
|
technical difficulties
production problems
|
|
gptkbp:compressionRatio
|
6.5:1
|
|
gptkbp:configuration
|
24-cylinder
six-bank
|
|
gptkbp:coolingSystem
|
liquid-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:Germany
|
|
gptkbp:developedBy
|
1937–1944
|
|
gptkbp:displacement
|
46.4 L
|
|
gptkbp:engineType
|
liquid-cooled
inline engine
|
|
gptkbp:firstFlight
|
1939
|
|
gptkbp:fuelType
|
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Jumo 222 engines
|
|
gptkbp:intendedUse
|
gptkb:aircraft
|
|
gptkbp:manufacturer
|
gptkb:Junkers
|
|
gptkbp:notableFeature
|
compact design
high power-to-weight ratio
|
|
gptkbp:notableProject
|
gptkb:Bomber_B_program
|
|
gptkbp:numberBuilt
|
less than 300
|
|
gptkbp:powerOutput
|
2,500–3,000 hp
|
|
gptkbp:predecessor
|
gptkb:Jumo_211
|
|
gptkbp:projectCancelled
|
1944
|
|
gptkbp:rpm
|
3,200 rpm
|
|
gptkbp:status
|
experimental
limited production
|
|
gptkbp:stroke
|
140 mm
|
|
gptkbp:successor
|
none
|
|
gptkbp:supercharger
|
two-stage
|
|
gptkbp:usedDuring
|
gptkb:World_War_II
|
|
gptkbp:usedIn
|
gptkb:Focke-Wulf_Ta_152
gptkb:Junkers_Ju_388
gptkb:Junkers_Ju_488
gptkb:Dornier_Do_317
gptkb:Junkers_Ju_288
|
|
gptkbp:weight
|
1,350 kg
|
|
gptkbp:bfsParent
|
gptkb:Junkers_Ju_488
|
|
gptkbp:bfsLayer
|
7
|