Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
6.0 in
|
| gptkbp:compressionRatio |
7:1
|
| gptkbp:configuration |
liquid-cooled
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
36.7 litres
|
| gptkbp:engineType |
V-12 piston engine
|
| gptkbp:firstFlight |
1940s
|
| gptkbp:fuelType |
100 octane aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Griffon 59
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notableFeature |
improved high-altitude performance
|
| gptkbp:powerOutput |
2,450 hp
|
| gptkbp:propulsion |
contra-rotating propellers
|
| gptkbp:stroke |
6.6 in
|
| gptkbp:supercharger |
two-stage, two-speed
|
| gptkbp:usedIn |
gptkb:Supermarine_Seafire
gptkb:Supermarine_Spitfire_Mk_XIX |
| gptkbp:valvetrain |
overhead camshaft
|
| gptkbp:weight |
2,050 lb
|
| gptkbp:bfsParent |
gptkb:Fairey_Firefly_TT.20
|
| gptkbp:bfsLayer |
6
|