Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
5 in
|
| gptkbp:configuration |
H-24
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
2,467 cubic inches
|
| gptkbp:firstRun |
1933
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:manufacturer |
gptkb:Napier_&_Son
|
| gptkbp:numberOfEngines |
24
|
| gptkbp:powerOutput |
up to 1,000 hp
|
| gptkbp:status |
retired
|
| gptkbp:stroke |
3.5 in
|
| gptkbp:successor |
gptkb:Napier_Sabre
|
| gptkbp:usedInAircraft |
gptkb:Fairey_Battle
gptkb:Hawker_Hector Blackburn B.26 Botha |
| gptkbp:valveConfiguration |
sleeve valve
|
| gptkbp:bfsParent |
gptkb:Frank_Halford
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
Napier Dagger engine
|