Pratt & Whitney R-1340 Wasp
GPTKB entity
Statements (79)
Predicate | Object |
---|---|
gptkbp:instance_of |
gptkb:jet_engine
|
gptkbp:aircraft_operated |
gptkb:Douglas_DC-3
gptkb:Grumman_F4_F_Wildcat gptkb:North_American_T-6_Texan gptkb:Boeing_Stearman_PT-17 gptkb:Lockheed_Vega |
gptkbp:application |
gptkb:transport_aircraft
gptkb:aircraft gptkb:trainer_aircraft crop dusting aerial firefighting |
gptkbp:compression_ratio |
6.5:1
6:1 |
gptkbp:configuration |
9-cylinder
|
gptkbp:cooling_system |
air-cooled
|
gptkbp:displacement |
1,340 cubic inches
1340 cubic inches |
gptkbp:engine |
gptkb:Wasp_series
lightweight construction military and civilian aircraft four-stroke high power-to-weight ratio robust design versatile applications Wasp family good fuel efficiency historical significance in aviation simple maintenance proven performance widely used in aviation |
gptkbp:engine_configuration |
horizontally opposed
front-mounted radial layout two-row radial radial configuration R-1340 |
gptkbp:engine_power |
high reliability
600 horsepower 2200 RPM |
gptkbp:engine_type |
piston engine
reciprocating engine R-1340-AN-1 R-1340-AN-3 R-1340-AN-6 R-1340-AN-7 R-1340-AN-10 R-1340-AN-2 R-1340-AN-4 R-1340-AN-5 R-1340-AN-8 R-1340-AN-9 |
gptkbp:first_flight |
1925
|
gptkbp:fuel_capacity |
3 ft 6 in
4 ft 6 in 2 ft 6 in |
gptkbp:fuel_type |
aviation gasoline
carbureted |
https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney R-1340 Wasp
|
gptkbp:ignition_system |
dual ignition
|
gptkbp:maintenance |
periodic inspections
|
gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
gptkbp:original_run |
1925
|
gptkbp:power_output |
600 hp
600 horsepower |
gptkbp:production_years |
1925-1940
1925 to 1940s |
gptkbp:propeller |
variable-pitch propeller
|
gptkbp:successor |
gptkb:Pratt_&_Whitney_R-985_Wasp_Junior
|
gptkbp:torque |
300 lb-ft
wet sump |
gptkbp:type |
gptkb:radial_engine
|
gptkbp:used_in |
gptkb:military_aircraft
civilian aircraft various aircraft |
gptkbp:valve_configuration |
overhead valves
|
gptkbp:weight |
about 600 pounds
about 600 lb |
gptkbp:bfsParent |
gptkb:Boeing_P-26_Peashooter
|
gptkbp:bfsLayer |
4
|