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