Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
5.4 in
|
| gptkbp:compressionRatio |
6.5:1
|
| gptkbp:configuration |
gptkb:X-24
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:discontinued |
reliability problems
|
| gptkbp:displacement |
42 litres
|
| gptkbp:engineType |
liquid-cooled V-24 piston engine
|
| gptkbp:firstFlight |
1937
|
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Vulture
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notableFeature |
X-24 configuration
intended for heavy bombers |
| gptkbp:numberBuilt |
538
|
| gptkbp:powerOutput |
1,800 hp
|
| gptkbp:productionStartYear |
1937–1941
|
| gptkbp:status |
discontinued
|
| gptkbp:stroke |
5.5 in
|
| gptkbp:successor |
gptkb:Rolls-Royce_Merlin
|
| gptkbp:usedInAircraft |
gptkb:Avro_Manchester
gptkb:Vickers_Warwick gptkb:Hawker_Tornado |
| gptkbp:valvetrain |
DOHC, 4 valves per cylinder
|
| gptkbp:weight |
1,640 lb
|
| gptkbp:bfsParent |
gptkb:Avro_Manchester
|
| gptkbp:bfsLayer |
5
|