Bristol Hercules 230 radial engines
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:configuration |
two-row radial
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
38.7 L
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:firstFlight |
1939
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:manufacturer |
gptkb:Bristol_Aeroplane_Company
|
| gptkbp:notableFeature |
high reliability
sleeve valve design used extensively in WWII |
| gptkbp:numberOfEngines |
14
|
| gptkbp:powerOutput |
~2,000 hp
|
| gptkbp:usedIn |
gptkb:Vickers_Wellington
gptkb:aircraft gptkb:Short_Stirling gptkb:Bristol_Beaufighter Avro Lancaster (some variants) |
| gptkbp:bfsParent |
gptkb:Vickers_Valetta
gptkb:Valetta_C.1 |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bristol Hercules 230 radial engines
|