|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:Boeing_B-17_Flying_Fortress
gptkb:P-51_Mustang
gptkb:C-46_Commando
gptkb:P-47_Thunderbolt
gptkb:B-24_Liberator
|
|
gptkbp:bore
|
5.5 inches
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:displacement
|
975 cubic inches
|
|
gptkbp:engine
|
gptkb:Continental_R-1340
gptkb:series
gptkb:Racing
reduction gear
Continental R engine family
Continental R-790
Continental R-9
|
|
gptkbp:engine_configuration
|
horizontally opposed
radial layout
|
|
gptkbp:engine_power
|
high reliability
high power-to-weight ratio
long lifespan
maximum RPM of 2800
|
|
gptkbp:engine_type
|
reciprocating engine
R975-AN-1
R975-AN-10
R975-AN-2
R975-AN-3
R975-AN-4
R975-AN-5
R975-AN-6
R975-AN-7
R975-AN-8
R975-AN-9
|
|
gptkbp:first_introduced
|
gptkb:1940
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Continental R975
|
|
gptkbp:ignition_system
|
dual ignition
|
|
gptkbp:maintenance
|
moderate maintenance requirements
|
|
gptkbp:manufacturer
|
gptkb:Continental_Motors
|
|
gptkbp:number_of_engines
|
9 cylinders
|
|
gptkbp:number_of_strokes
|
4-stroke
|
|
gptkbp:power_output
|
400 horsepower
|
|
gptkbp:production_years
|
1940-1950
|
|
gptkbp:stroke
|
6.0 inches
|
|
gptkbp:successor
|
Continental R-670
|
|
gptkbp:torque
|
high torque output
|
|
gptkbp:type
|
gptkb:radial_engine
|
|
gptkbp:used_in
|
gptkb:military_aircraft
|
|
gptkbp:valve_configuration
|
pushrod
|
|
gptkbp:weight
|
approximately 600 pounds
|
|
gptkbp:bfsParent
|
gptkb:M-4
gptkb:M4
|
|
gptkbp:bfsLayer
|
5
|