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gptkbp:instanceOf
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aircraft engine
|
|
gptkbp:aircraft
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gptkb:Lockheed_Model_10_Electra
gptkb:Douglas_DC-2
|
|
gptkbp:application
|
military aviation
civil aviation
|
|
gptkbp:bore
|
5.5 inches
|
|
gptkbp:compressionRatio
|
6:1
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|
gptkbp:controls
|
mechanical throttle
|
|
gptkbp:coolingSystem
|
air-cooled
direct air cooling
|
|
gptkbp:cylinderCount
|
9
|
|
gptkbp:design
|
gptkb:Wright_Aeronautical_Corporation
|
|
gptkbp:displacement
|
1,300 cubic inches
|
|
gptkbp:drivetrain
|
pushrod actuated
|
|
gptkbp:engine
|
horizontally opposed
front-mounted
|
|
gptkbp:engineConfiguration
|
9-cylinder radial
|
|
gptkbp:engineType
|
R-1300-1
R-1300-10
R-1300-2
R-1300-3
R-1300-4
R-1300-5
R-1300-6
R-1300-7
R-1300-8
R-1300-9
|
|
gptkbp:firstFlight
|
1930
|
|
gptkbp:fuelType
|
aviation gasoline
carbureted
dual ignition
|
|
gptkbp:hasArea
|
extensive ground testing
FAA_certified
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Wright R-1300
|
|
gptkbp:manufacturer
|
gptkb:Wright_Aeronautical_Corporation
|
|
gptkbp:notableUsers
|
gptkb:Transcontinental_&_Western_Air
gptkb:Pan_American_Airways
gptkb:United_States_Army_Air_Corps
|
|
gptkbp:performances
|
high reliability
approximately 1,500 hours
moderate complexity
|
|
gptkbp:powerOutput
|
600 horsepower
|
|
gptkbp:productionYears
|
1930-1935
|
|
gptkbp:propulsion
|
variable pitch
|
|
gptkbp:related_engine
|
gptkb:Wright_R-1300_family
|
|
gptkbp:setting
|
radial
|
|
gptkbp:stroke
|
6.0 inches
|
|
gptkbp:successor
|
gptkb:Wright_R-1820
|
|
gptkbp:type
|
radial engine
|
|
gptkbp:weight
|
approximately 600 pounds
|