Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft_engine_variant
|
| gptkbp:application |
heavy bombers
|
| 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
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notableFeature |
improved high-altitude performance
|
| gptkbp:powerOutput |
1,620 hp
|
| gptkbp:supercharger |
two-stage, two-speed
|
| gptkbp:usedIn |
gptkb:aircraft
gptkb:Short_Stirling |
| gptkbp:bfsParent |
gptkb:Avro_Lancaster_B.VII
|
| gptkbp:bfsLayer |
9
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Merlin 24 or 38
|