Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
152.4 mm
|
| gptkbp:compressionRatio |
6:1
|
| gptkbp:configuration |
V-12
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:designer |
gptkb:Arthur_Rowledge
|
| gptkbp:displacement |
36.7 L
|
| gptkbp:firstFlight |
1929
|
| gptkbp:fuelType |
petrol
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:museumDisplay |
gptkb:Science_Museum,_London
gptkb:Royal_Air_Force_Museum_Cosford |
| gptkbp:notableFor |
winning the Schneider Trophy
influencing the design of the Rolls-Royce Merlin |
| gptkbp:numberBuilt |
19
|
| gptkbp:powerOutput |
2,300 hp
|
| gptkbp:purpose |
air racing
|
| gptkbp:status |
retired
|
| gptkbp:stroke |
169.9 mm
|
| gptkbp:usedIn |
gptkb:Supermarine_S.6B
gptkb:Supermarine_S.6 gptkb:Gloster_IV gptkb:Supermarine_S.6A |
| gptkbp:weight |
1,640 lb
|
| gptkbp:bfsParent |
gptkb:Supermarine_S.6
|
| gptkbp:bfsLayer |
8
|
| http://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce R
|