Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
5 in (127 mm)
|
| gptkbp:configuration |
H-24
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
2,238 cu in (36.6 L)
|
| gptkbp:engineType |
liquid-cooled H-24 piston engine
|
| gptkbp:firstFlight |
1940s
|
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Napier Sabre II
|
| gptkbp:manufacturer |
gptkb:Napier_&_Son
|
| gptkbp:notableFor |
high power-to-weight ratio
|
| gptkbp:powerOutput |
2,200 hp
|
| gptkbp:predecessor |
Napier Sabre I
|
| gptkbp:stroke |
4.75 in (121 mm)
|
| gptkbp:successor |
gptkb:Napier_Sabre_IIA
|
| gptkbp:usedInAircraft |
gptkb:Hawker_Tempest
gptkb:Hawker_Typhoon |
| gptkbp:valvetrain |
sleeve valve
|
| gptkbp:bfsParent |
gptkb:Tempest_Mk_V
|
| gptkbp:bfsLayer |
7
|