Statements (21)
| 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:firstFlight |
1938
|
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Merlin X
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:powerOutput |
1,130 hp
|
| gptkbp:relatedTo |
Rolls-Royce Merlin engine family
|
| gptkbp:stroke |
6.0 in
|
| gptkbp:supercharger |
single-stage, two-speed
|
| gptkbp:usedIn |
gptkb:Armstrong_Whitworth_Whitley
gptkb:Vickers_Wellington gptkb:Fairey_Battle |
| gptkbp:weight |
1,640 lb
|
| gptkbp:bfsParent |
gptkb:Halifax_B_Mk_I
|
| gptkbp:bfsLayer |
5
|