Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
5.75 in
|
| gptkbp:compressionRatio |
6.5:1
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
950 cubic inches
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:firstRun |
1934
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:manufacturer |
gptkb:Bristol_Aeroplane_Company
|
| gptkbp:notableFeature |
sleeve valve design
|
| gptkbp:numberOfEngines |
9
|
| gptkbp:powerOutput |
500 hp
|
| gptkbp:predecessor |
gptkb:Bristol_Mercury_engine
|
| gptkbp:status |
experimental
|
| gptkbp:stroke |
6.5 in
|
| gptkbp:successor |
gptkb:Bristol_Perseus_engine
|
| gptkbp:usedInAircraft |
gptkb:Bristol_Type_143
gptkb:Fairey_P.4/34 |
| gptkbp:weight |
850 lb
|
| gptkbp:bfsParent |
gptkb:Aerospace_Bristol
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
Bristol Aquila engine
|