|
gptkbp:instanceOf
|
aircraft engine
|
|
gptkbp:compressionRatio
|
5.5:1
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:displacement
|
1,200 cubic inches
|
|
gptkbp:engine
|
commercial aviation
military aviation
fighter aircraft
bomber aircraft
civil aviation
transport aircraft
training aircraft
reconnaissance aircraft
horizontally opposed
seaplane
passenger aircraft
cargo_aircraft
Wright_design
|
|
gptkbp:engineConfiguration
|
aircraft engine configuration
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1925
|
|
gptkbp:fuelType
|
aviation gasoline
dual ignition
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Wright J-5 series
|
|
gptkbp:is_used_in
|
gptkb:Douglas_DC-3
gptkb:Boeing_40
gptkb:Wright_Flyer
|
|
gptkbp:manufacturer
|
gptkb:Wright_Aeronautical_Corporation
|
|
gptkbp:notableUsers
|
gptkb:Transcontinental_and_Western_Air
gptkb:Pan_American_Airways
gptkb:United_States_Navy
gptkb:United_States_Army_Air_Service
|
|
gptkbp:powerOutput
|
300 horsepower
|
|
gptkbp:productionYears
|
1925 to 1940
|
|
gptkbp:propulsion
|
variable pitch propeller
|
|
gptkbp:related_engine
|
gptkb:Wright_J_series
gptkb:Wright_R-1300_family
|
|
gptkbp:setting
|
9 cylinders
|
|
gptkbp:successor
|
gptkb:Wright_R-1300
|
|
gptkbp:type
|
radial engine
|
|
gptkbp:weight
|
approximately 600 pounds
|