Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:applicationEra |
gptkb:World_War_II
|
| gptkbp:configuration |
H-type
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
2,238 cubic inches
|
| gptkbp:engineType |
liquid-cooled
H-24 |
| gptkbp:firstFlight |
1940s
|
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Napier Sabre IIB
|
| gptkbp:manufacturer |
gptkb:Napier_&_Son
|
| gptkbp:numberOfEngines |
24
|
| gptkbp:powerOutput |
2,400 hp
|
| gptkbp:supercharger |
two-stage
|
| gptkbp:usedInAircraft |
gptkb:Hawker_Tempest
gptkb:Hawker_Typhoon |
| gptkbp:valveConfiguration |
sleeve valve
|
| gptkbp:bfsParent |
gptkb:Tempest_Mk_VI
|
| gptkbp:bfsLayer |
7
|