Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
5.0 in (127 mm)
|
| gptkbp:configuration |
H-24
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
36.7 litres
|
| gptkbp:engineType |
liquid-cooled H-24 piston engine
|
| gptkbp:firstFlight |
1938
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:manufacturer |
gptkb:Napier_&_Son
|
| gptkbp:notableFor |
high power-to-weight ratio
complex sleeve valve design use in British fighter-bombers |
| gptkbp:notableVariant |
Sabre II
Sabre IIA Sabre V Sabre VII |
| gptkbp:numberOfEngines |
24
|
| gptkbp:powerOutput |
over 2,000 hp
|
| gptkbp:productionStartYear |
1940s
|
| gptkbp:stroke |
4.75 in (121 mm)
|
| gptkbp:usedDuring |
gptkb:World_War_II
|
| gptkbp:usedInAircraft |
gptkb:Hawker_Tempest
gptkb:Hawker_Typhoon gptkb:Blackburn_Firebrand |
| gptkbp:weight |
2,360 lb (1,070 kg)
|
| gptkbp:bfsParent |
gptkb:D._Napier_&_Son
gptkb:Frank_Halford |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Napier Sabre engine
|