Statements (23)
Predicate | Object |
---|---|
gptkbp:instanceOf |
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 |
piston engine
|
gptkbp:firstRun |
1934
|
gptkbp:fuelType |
aviation gasoline
|
https://www.w3.org/2000/01/rdf-schema#label |
Bristol Aquila engine
|
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 |
6
|