Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
5.4 in
|
| gptkbp:compressionRatio |
6.0:1
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
27 litres
|
| gptkbp:engineType |
V-12 piston engine
|
| gptkbp:firstFlight |
1936
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:powerOutput |
1,030 hp
|
| gptkbp:predecessor |
gptkb:Rolls-Royce_Kestrel
|
| gptkbp:stroke |
6.0 in
|
| gptkbp:successor |
gptkb:Rolls-Royce_Merlin_XX
|
| gptkbp:supercharger |
single-stage
|
| gptkbp:usedDuring |
gptkb:World_War_II
|
| gptkbp:usedIn |
gptkb:aircraft
gptkb:Hawker_Hurricane |
| gptkbp:valvetrain |
DOHC, 4 valves per cylinder
|
| gptkbp:weight |
1,335 lb
|
| gptkbp:bfsParent |
gptkb:Supermarine_Type_300
gptkb:the_Spitfire_prototype |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Merlin C
|