Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
6.0 in (152 mm)
|
| gptkbp:configuration |
60° V12
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:developedBy |
gptkb:Rolls-Royce_R_engine
|
| gptkbp:displacement |
36.7 litres
|
| gptkbp:engineType |
liquid-cooled V12 piston engine
|
| gptkbp:firstFlight |
1930
|
| gptkbp:fuelType |
petrol
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:numberBuilt |
100
|
| gptkbp:powerOutput |
800-955 hp
|
| gptkbp:status |
retired
|
| gptkbp:stroke |
6.6 in (168 mm)
|
| gptkbp:usedInAircraft |
Short Singapore II
Supermarine S.6B (prototype) |
| gptkbp:bfsParent |
gptkb:Rolls-Royce_R_engine
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Buzzard
|