Properties (55)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft engine
|
| gptkbp:aircraft |
gptkb:Douglas_DC-3
gptkb:Boeing_B-17_Flying_Fortress gptkb:North_American_B-25_Mitchell gptkb:Lockheed_P-38_Lightning gptkb:Curtiss_P-40_Warhawk |
| gptkbp:application |
fighter aircraft
bomber aircraft transport aircraft |
| gptkbp:compressionRatio |
6:1
|
| gptkbp:coolingSystem |
air-cooled
air-cooled radial |
| gptkbp:displacement |
1,300 cubic inches
|
| gptkbp:drivetrain |
pushrod actuated
|
| gptkbp:engine |
approximately 30 inches
approximately 60 inches approximately 50 inches radial layout influenced future engine designs various military applications various civilian applications |
| gptkbp:engineConfiguration |
horizontally opposed
produced in large numbers |
| gptkbp:engineType |
multiple variants produced
|
| gptkbp:firstFlight |
1930s
|
| gptkbp:fuelType |
aviation gasoline
dual ignition |
| https://www.w3.org/2000/01/rdf-schema#label |
Wright R-1300 family
|
| gptkbp:is_used_in |
military aircraft
civil aircraft |
| gptkbp:manufacturer |
gptkb:Wright_Aeronautical_Corporation
|
| gptkbp:notable_feature |
R-1300-1
R-1300-3 |
| gptkbp:operationalHistory |
gptkb:Korean_War
gptkb:World_War_II |
| gptkbp:performances |
high durability
smooth operation high reliability high power-to-weight ratio low vibration levels robust design versatile applications good fuel efficiency moderate maintenance requirements easy to repair good throttle response |
| gptkbp:powerOutput |
600 to 700 horsepower
|
| gptkbp:productionYears |
1930s to 1940s
|
| gptkbp:related_engine |
gptkb:Wright_radial_engines
gptkb:Wright_R-1300_series |
| gptkbp:replacedBy |
gptkb:Wright_R-1820
|
| gptkbp:setting |
14-cylinder
|
| gptkbp:successor |
gptkb:Wright_R-1300-5
|
| gptkbp:type |
radial engine
|
| gptkbp:weight |
approximately 800 pounds
|