Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
6.0 in
|
| gptkbp:compressionRatio |
7:1
|
| gptkbp:configuration |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
36.7 litres
|
| gptkbp:engineType |
V-12 piston engine
|
| gptkbp:firstFlight |
1945
|
| gptkbp:fuelType |
100 octane aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Griffon 83
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:powerOutput |
2,350 hp
|
| gptkbp:propulsion |
contra-rotating propellers
|
| gptkbp:stroke |
6.6 in
|
| gptkbp:supercharger |
two-stage, two-speed
|
| gptkbp:usedIn |
gptkb:Supermarine_Spitfire_Mk_24
Supermarine Seafire Mk 47 |
| gptkbp:bfsParent |
gptkb:Martin-Baker_MB_5
|
| gptkbp:bfsLayer |
6
|