Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
5.75 in
|
| gptkbp:compressionRatio |
7.0:1
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
1,520 cu in
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:firstRun |
1932
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:manufacturer |
gptkb:Bristol_Aeroplane_Company
|
| gptkbp:notableFor |
first successful sleeve valve aero engine
|
| gptkbp:numberOfEngines |
9
|
| gptkbp:powerOutput |
up to 930 hp
|
| gptkbp:predecessor |
gptkb:Bristol_Jupiter
|
| gptkbp:productionStartYear |
1932–1940s
|
| gptkbp:stroke |
6.5 in
|
| gptkbp:successor |
gptkb:Bristol_Hercules
|
| gptkbp:usedInAircraft |
gptkb:Bristol_Beaufort
gptkb:Bristol_Bombay gptkb:Short_Sunderland gptkb:Fairey_Albacore |
| gptkbp:weight |
1,030 lb
|
| gptkbp:bfsParent |
gptkb:De_Havilland_Flamingo
gptkb:Bristol_Aero_Engines gptkb:Bristol_Taurus_radial_engine |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bristol Perseus
|