Statements (52)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:aircraft_operated |
gptkb:Douglas_DC-3
gptkb:Lockheed_Electra gptkb:Boeing_307_Stratoliner |
| gptkbp:application |
gptkb:military_aircraft
commercial aviation |
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:configuration |
air-cooled
|
| gptkbp:cooling_system |
air-cooled
air-cooled radial |
| gptkbp:displacement |
1300 cubic inches
|
| gptkbp:engine |
gptkb:Wright_R-1300_series
reliable performance part of aviation history produced in large numbers influenced future engine designs used in various aircraft types incorporated innovative technologies historically significant in aviation developed during the 1930s distinctive design features present operational use in various conditions |
| gptkbp:engine_configuration |
radial
robust design horizontally opposed detailed specifications available Wright Aeronautical design |
| gptkbp:engine_power |
high reliability
high power-to-weight ratio measured performance metrics available |
| gptkbp:engine_production_numbers |
high production numbers achieved
|
| gptkbp:engine_type |
piston engine
multiple variants available |
| gptkbp:first_flight |
1930s
|
| gptkbp:fuel_type |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Wright R-1300 family
|
| gptkbp:ignition_system |
dual ignition
|
| gptkbp:is_tested_for |
extensively tested before production
|
| gptkbp:maintenance |
moderate maintenance requirements
|
| gptkbp:manufacturer |
gptkb:Wright_Aeronautical_Corporation
|
| gptkbp:number_of_engines |
gptkb:9
|
| gptkbp:power_output |
600 to 700 horsepower
|
| gptkbp:production_years |
1930s to 1940s
|
| gptkbp:replaced_by |
gptkb:Wright_R-1820
|
| gptkbp:successor |
gptkb:Wright_R-1820
|
| gptkbp:type |
gptkb:radial_engine
|
| gptkbp:used_in |
gptkb:military_aircraft
civil aircraft |
| gptkbp:valve_configuration |
pushrod operated
|
| gptkbp:weight |
approximately 800 pounds
|
| gptkbp:bfsParent |
gptkb:Wright_R-1300
|
| gptkbp:bfsLayer |
6
|