Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
5.4 in
|
| gptkbp:compressionRatio |
6.0:1
|
| gptkbp:configuration |
V-12
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
27 litres
|
| gptkbp:firstFlight |
1942
|
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Merlin 61
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notableFeature |
improved high-altitude performance
|
| gptkbp:partOf |
Rolls-Royce Merlin engine family
|
| gptkbp:powerOutput |
1565 hp
|
| gptkbp:predecessor |
gptkb:Merlin_45
|
| gptkbp:stroke |
6.0 in
|
| gptkbp:successor |
Merlin 63
|
| gptkbp:supercharger |
two-stage, two-speed
|
| gptkbp:usedIn |
gptkb:De_Havilland_Mosquito
gptkb:Supermarine_Spitfire_Mk_IX |
| gptkbp:weight |
1640 lb
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Merlin_engines
|
| gptkbp:bfsLayer |
6
|