Pratt & Whitney R-1340 Wasp Junior

URI: https://gptkb.org/entity/Pratt_%26_Whitney_R-1340_Wasp_Junior
GPTKB entity
Statements (52)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:bfsLayer 6
gptkbp:bfsParent gptkb:Double_Wasp
gptkbp:aircraft_operated gptkb:Douglas_DC-3
gptkb:Grumman_F4_F_Wildcat
gptkb:Boeing_Stearman_PT-17
gptkb:Lockheed_Electra_10
gptkbp:compression_ratio 6.5:1
gptkbp:cooling_system air-cooled
gptkbp:displacement 1340 cubic inches
gptkbp:engine four-stroke
radial
horizontally opposed
Wasp family
R-1340-AN-1
R-1340-AN-17
R-1340-AN-3
R-1340-AN-6
R-1340-AN-7
R-1340 series
R-1340-AN-10
R-1340-AN-11
R-1340-AN-12
R-1340-AN-13
R-1340-AN-14
R-1340-AN-15
R-1340-AN-16
R-1340-AN-18
R-1340-AN-19
R-1340-AN-2
R-1340-AN-20
R-1340-AN-4
R-1340-AN-5
R-1340-AN-8
R-1340-AN-9
gptkbp:engine_type reciprocating engine
gptkbp:first_flight 1925
gptkbp:fuel_type aviation gasoline
carbureted
https://www.w3.org/2000/01/rdf-schema#label Pratt & Whitney R-1340 Wasp Junior
gptkbp:ignition_system dual ignition
gptkbp:is_designed_to civil and military aviation
gptkbp:manufacturer gptkb:Pratt_&_Whitney
gptkbp:power_output 600 horsepower
gptkbp:production_years 1925-1960
gptkbp:propulsion variable-pitch propeller
gptkbp:setting 9-cylinder
gptkbp:successor gptkb:Pratt_&_Whitney_R-985_Wasp_Junior
gptkbp:type gptkb:engine
gptkbp:used_in gptkb:aircraft
gptkbp:valve_configuration overhead valves
gptkbp:weight 350 pounds