Properties (43)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft engine
|
| gptkbp:application |
military aircraft
civil aircraft |
| gptkbp:bore |
5.5 inches
|
| gptkbp:compressionRatio |
6.5:1
|
| gptkbp:coolingSystem |
air-cooled
air-cooled radial |
| gptkbp:cylinderCount |
14 cylinders
|
| gptkbp:displacement |
1,300 cubic inches
|
| gptkbp:drivetrain |
pushrod actuated
|
| gptkbp:engine |
influenced future designs
radial layout Wright_design |
| gptkbp:engineConfiguration |
limited production
horizontally opposed |
| gptkbp:engineType |
reciprocating engine
|
| gptkbp:firstFlight |
1930s
|
| gptkbp:fuelType |
aviation gasoline
dual ignition |
| https://www.w3.org/2000/01/rdf-schema#label |
Wright R-1300 engine
|
| gptkbp:is_used_in |
gptkb:C-46_Commando
B-17 Flying Fortress B-24 Liberator |
| gptkbp:manufacturer |
gptkb:Wright_Aeronautical_Corporation
|
| gptkbp:notable_feature |
high power-to-weight ratio
reliable performance robust design |
| gptkbp:operationalHistory |
historically significant engine
|
| gptkbp:performances |
high reliability
moderate maintenance requirements detailed specifications available. high_altitude_performance |
| gptkbp:powerOutput |
1,000 horsepower
|
| gptkbp:productionYears |
1930s to 1940s
|
| gptkbp:propulsion |
variable pitch
|
| gptkbp:related_engine |
gptkb:Wright_R-1600_engine
gptkb:Wright_R-1820_engine gptkb:Wright_R-1200_engine gptkb:Wright_R-1300_family |
| gptkbp:stroke |
6.0 inches
|
| gptkbp:successor |
gptkb:Wright_R-1820_engine
|
| gptkbp:type |
radial engine
|
| gptkbp:weight |
approximately 1,200 pounds
|