|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:bore
|
4 inches
|
|
gptkbp:compressionRatio
|
4.9:1
|
|
gptkbp:configuration
|
gptkb:upright_V8
|
|
gptkbp:coolingSystem
|
liquid-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:displacement
|
502 cubic inches
|
|
gptkbp:engineType
|
gptkb:V8
|
|
gptkbp:firstFlight
|
1910s
|
|
gptkbp:fuelType
|
gptkb:gasoline
carburetor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Curtiss OX-5
|
|
gptkbp:ignition
|
dual magneto
|
|
gptkbp:manufacturer
|
gptkb:Curtiss_Aeroplane_and_Motor_Company
|
|
gptkbp:notableFor
|
first mass-produced American aircraft engine
widely used in World War I trainers
|
|
gptkbp:powerOutput
|
90 hp
|
|
gptkbp:productionStartYear
|
1915–1919
|
|
gptkbp:rpm
|
1400
|
|
gptkbp:stroke
|
5 inches
|
|
gptkbp:successor
|
gptkb:Curtiss_OX-6
|
|
gptkbp:usedInAircraft
|
gptkb:Alexander_Eaglerock
gptkb:Standard_J-1
gptkb:Travel_Air_2000
gptkb:Curtiss_JN-4
gptkb:Waco_9
|
|
gptkbp:valveConfiguration
|
side-valve
|
|
gptkbp:weight
|
390 lbs
|
|
gptkbp:bfsParent
|
gptkb:Swallow_biplane
gptkb:Curtiss_Model_K
gptkb:Curtiss_Model_L
gptkb:Curtiss_No._39
gptkb:Curtiss_No._49
gptkb:Curtiss_No._50
gptkb:Epps_1912_Monoplane
|
|
gptkbp:bfsLayer
|
7
|