gptkbp:instance_of
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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
|