R-1340 Wasp

GPTKB entity

Statements (59)
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:Curtiss_P-40_Warhawk
gptkbp:application gptkb:transport_aircraft
gptkb:aircraft
gptkb:trainer_aircraft
gptkb:fighter_aircraft
gptkbp:compression_ratio 6.5:1
gptkbp:configuration single-row
gptkbp:cooling_system air-cooled
air-cooled radial
gptkbp:displacement 1,340 cubic inches
gptkbp:engine gptkb:Wasp_series
Wasp family
over 30,000 units
gptkbp:engine_configuration horizontally opposed
9-cylinder radial
gptkbp:engine_type reciprocating engine
R-1340-5
R-1340-6
R-1340-4
R-1340-18
R-1340-7
R-1340-1
R-1340-10
R-1340-11
R-1340-12
R-1340-13
R-1340-14
R-1340-15
R-1340-16
R-1340-17
R-1340-19
R-1340-2
R-1340-20
R-1340-3
R-1340-8
R-1340-9
gptkbp:fuel_type aviation gasoline
https://www.w3.org/2000/01/rdf-schema#label R-1340 Wasp
gptkbp:ignition_system dual ignition
gptkbp:manufacturer gptkb:Pratt_&_Whitney
gptkbp:number_of_engines 9 cylinders
gptkbp:original_run 1925
gptkbp:power_output 600 horsepower
gptkbp:production_years 1925-1945
gptkbp:propeller variable-pitch propeller
gptkbp:successor gptkb:R-1830_Twin_Wasp
gptkbp:successor_engine R-1340-AN
gptkbp:type gptkb:radial_engine
gptkbp:used_in gptkb:military_aircraft
civilian aircraft
gptkbp:valve_configuration overhead valves
gptkbp:weight about 600 pounds
gptkbp:bfsParent gptkb:H-1_radial_engine
gptkbp:bfsLayer 6