|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:basedOn
|
gptkb:Rolls-Royce_Merlin
|
|
gptkbp:bore
|
5.4 in
|
|
gptkbp:compressionRatio
|
6.0:1
|
|
gptkbp:configuration
|
V-12
|
|
gptkbp:coolingSystem
|
liquid-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:displacement
|
1650 cubic inches
|
|
gptkbp:firstFlight
|
1942
|
|
gptkbp:fuelType
|
aviation gasoline
carburetor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Packard V-1650 Merlin
|
|
gptkbp:ignition
|
dual magneto
|
|
gptkbp:manufacturer
|
gptkb:Packard
|
|
gptkbp:notableFor
|
enabling high-altitude performance in P-51 Mustang
|
|
gptkbp:notableUser
|
gptkb:Royal_Air_Force
gptkb:United_States_Army_Air_Forces
|
|
gptkbp:numberBuilt
|
over 55,000
|
|
gptkbp:powerOutput
|
up to 1,720 hp
|
|
gptkbp:predecessor
|
gptkb:Rolls-Royce_Merlin
|
|
gptkbp:productionStartYear
|
1941–1946
|
|
gptkbp:stroke
|
6.0 in
|
|
gptkbp:successor
|
none
|
|
gptkbp:supercharger
|
two-stage
|
|
gptkbp:usedDuring
|
gptkb:World_War_II
|
|
gptkbp:usedInAircraft
|
gptkb:aircraft
gptkb:Curtiss_P-40F
|
|
gptkbp:valvetrain
|
single overhead camshaft per bank
|
|
gptkbp:weight
|
1,640 lb
|
|
gptkbp:bfsParent
|
gptkb:North_American_P-51B/C_Mustang
|
|
gptkbp:bfsLayer
|
5
|