Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
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 |
liquid-cooled V12 piston engine
|
| gptkbp:family |
gptkb:Rolls-Royce_Merlin
|
| gptkbp:firstFlight |
1942
|
| gptkbp:fuelType |
100-octane aviation gasoline
carburettor |
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Merlin 55
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notableFeature |
improved high-altitude performance
|
| gptkbp:powerOutput |
1,455 hp
|
| gptkbp:stroke |
6.0 in
|
| gptkbp:supercharger |
single-stage, two-speed
|
| gptkbp:usedIn |
gptkb:Supermarine_Spitfire_Mk_XVI
gptkb:Supermarine_Spitfire_Mk_IX |
| gptkbp:valvetrain |
single overhead camshaft per bank
|
| gptkbp:weight |
1,640 lb
|
| gptkbp:bfsParent |
gptkb:Seafire_F_Mk_III
|
| gptkbp:bfsLayer |
7
|