Statements (50)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
engine
|
| gptkbp:compressionRatio |
6.5:1
|
| gptkbp:coolingSystem |
air-cooled
air-cooled radial |
| gptkbp:cylinderCount |
9 cylinders
|
| gptkbp:displacement |
975 cubic inches
|
| gptkbp:drivetrain |
pushrod actuated
|
| gptkbp:engine |
54 inches
military aviation 40 inches used in various aircraft models radial layout |
| gptkbp:engineConfiguration |
horizontally opposed
9-cylinder radial |
| gptkbp:engineType |
reciprocating engine
R975_C1-1 R975_C1-2 R975_C1-3 R975_C1-4 R975_C1-5 |
| gptkbp:fuelType |
aviation gasoline
carbureted dual ignition |
| gptkbp:hasArea |
extensive testing during development
|
| https://www.w3.org/2000/01/rdf-schema#label |
Continental R975 C1
|
| gptkbp:introduced |
1940s
|
| gptkbp:is_used_in |
military aircraft
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:maximum_speed |
2800 RPM
|
| gptkbp:notableFeature |
gptkb:C-54_Skymaster
gptkb:C-46_Commando B-17 Flying Fortress B-24 Liberator P-47 Thunderbolt |
| gptkbp:operationalHistory |
gptkb:Korean_War
gptkb:World_War_II important_in_WWII_aviation_history |
| gptkbp:performances |
high reliability
high power-to-weight ratio military specifications moderate maintenance requirements |
| gptkbp:powerOutput |
400 horsepower
|
| gptkbp:productionYears |
1940-1950s
|
| gptkbp:propulsion |
variable pitch
|
| gptkbp:related_engine |
gptkb:Continental_R_series
|
| gptkbp:replacedBy |
gptkb:Continental_R-1340
|
| gptkbp:successor |
gptkb:Continental_R-975_C1-1
|
| gptkbp:torque |
2000 lb-ft
|
| gptkbp:type |
radial engine
|
| gptkbp:weight |
approximately 600 pounds
|