|
gptkbp:instanceOf
|
aircraft engine
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:compressionRatio
|
6.5:1
|
|
gptkbp:coolingSystem
|
liquid cooling
liquid-cooled
water-cooled
|
|
gptkbp:displacement
|
1650 cubic inches
27 liters
|
|
gptkbp:drivetrain
|
overhead valve
|
|
gptkbp:engine
|
no
800 mm
1,200 mm
fighter aircraft
longitudinal
544 kg
V-1650-1
|
|
gptkbp:engineConfiguration
|
gptkb:Curtiss_Aeroplane_and_Motor_Company
gptkb:V-12_engine
gptkb:V-12
|
|
gptkbp:enginePower
|
1,200 kW
|
|
gptkbp:engineType
|
spark ignition
reciprocating engine
V-1650-7
|
|
gptkbp:firstFlight
|
1940
|
|
gptkbp:fuelType
|
spark ignition
aviation gasoline
carbureted
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Curtiss V-1650 Conqueror
|
|
gptkbp:is_used_in
|
gptkb:P-51_Mustang
P-47 Thunderbolt
|
|
gptkbp:manufacturer
|
gptkb:Curtiss_Aeroplane_and_Motor_Company
|
|
gptkbp:maximum_speed
|
3,000 RPM
|
|
gptkbp:operational_status
|
gptkb:P-51_Mustang
|
|
gptkbp:performances
|
high performance
high reliability
high efficiency
|
|
gptkbp:powerOutput
|
1,600 horsepower
|
|
gptkbp:productionYears
|
1940-1945
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:related_engine
|
Curtiss_V-1650_family
V-1650_series
|
|
gptkbp:setting
|
V engine
|
|
gptkbp:successor
|
Curtiss_V-1650-1
|
|
gptkbp:torque
|
1,200 lb-ft
1,600 Nm
|
|
gptkbp:type
|
gptkb:V-12_engine
|
|
gptkbp:weight
|
1,200 pounds
|