Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
5 in (127 mm)
|
| gptkbp:configuration |
H-type
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
36.7 litres
|
| gptkbp:engineType |
H-24 piston engine
|
| gptkbp:firstFlight |
1938
|
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Napier Sabre
|
| gptkbp:manufacturer |
gptkb:Napier_&_Son
|
| gptkbp:notableFor |
high power-to-weight ratio
complex sleeve valve design |
| gptkbp:numberOfEngines |
24
|
| gptkbp:powerOutput |
up to 3,500 hp
|
| gptkbp:predecessor |
gptkb:Napier_Lion
|
| gptkbp:productionStartYear |
1940–1946
|
| gptkbp:stroke |
4.75 in (121 mm)
|
| gptkbp:successor |
gptkb:Napier_Nomad
|
| gptkbp:usedDuring |
gptkb:World_War_II
|
| gptkbp:usedInAircraft |
gptkb:Hawker_Tempest
gptkb:Hawker_Typhoon gptkb:Martin-Baker_MB_3 gptkb:Blackburn_Firebrand |
| gptkbp:bfsParent |
gptkb:H_engine
gptkb:U_engine gptkb:Hawker_Tempest |
| gptkbp:bfsLayer |
6
|