Statements (51)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
engine
|
| gptkbp:bore |
5.5 inches
|
| gptkbp:compressionRatio |
6.5:1
|
| gptkbp:coolingSystem |
air-cooled
air-cooled radial |
| gptkbp:cylinderCount |
9 cylinders
|
| gptkbp:displacement |
16.0 liters
975 cubic inches |
| gptkbp:drivetrain |
pushrod actuated
|
| gptkbp:engine |
3.5 feet
World War II era 600 lbs 4.5 feet radial layout military aircraft engines 3.0 feet |
| gptkbp:engineConfiguration |
gptkb:Continental_Motors_Corporation
horizontally opposed 9-cylinder radial |
| gptkbp:enginePower |
400 hp at 2400 RPM
|
| gptkbp:engineType |
reciprocating engine
|
| gptkbp:fuel_capacity |
wet sump
|
| gptkbp:fuelType |
aviation gasoline
carbureted dual ignition |
| https://www.w3.org/2000/01/rdf-schema#label |
Continental R975
|
| gptkbp:introduced |
1930s
|
| gptkbp:is_used_in |
military aircraft
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:maximum_speed |
2800 RPM
|
| gptkbp:notableFeature |
gptkb:P-51_Mustang
gptkb:C-46_Commando B-17 Flying Fortress B-24 Liberator P-47 Thunderbolt |
| gptkbp:operationalHistory |
used_in_various_military_aircraft_during_WWII.
|
| gptkbp:performances |
high reliability
good performance at altitude moderate maintenance requirements |
| gptkbp:powerOutput |
400 horsepower
|
| gptkbp:productionYears |
1930s to 1940s
|
| gptkbp:propulsion |
variable pitch
|
| gptkbp:related_engine |
gptkb:Wright_R-975
gptkb:Pratt_&_Whitney_R-1340 R series |
| gptkbp:stroke |
6.0 inches
|
| gptkbp:successor |
gptkb:Continental_R-670
|
| gptkbp:torque |
2000 lb-ft
2000 lb-ft at 2000 RPM |
| gptkbp:type |
radial engine
|
| gptkbp:weight |
approximately 600 pounds
|