Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:basedOn |
gptkb:Rolls-Royce_Merlin
|
| gptkbp:bore |
5.4 in
|
| gptkbp:compressionRatio |
6.0:1
|
| gptkbp:configuration |
V-12
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:displacement |
1,649 cu in
|
| gptkbp:firstFlight |
1942
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:manufacturer |
gptkb:Packard
|
| gptkbp:powerOutput |
1,490 hp
|
| gptkbp:stroke |
6.0 in
|
| gptkbp:supercharger |
two-stage, two-speed
|
| gptkbp:usedDuring |
gptkb:World_War_II
|
| gptkbp:usedIn |
gptkb:Avro_Lancaster_(American-built_variants)
gptkb:de_Havilland_Mosquito_(American-built_variants) gptkb:aircraft |
| gptkbp:valvetrain |
DOHC, 4 valves per cylinder
|
| gptkbp:weight |
1,640 lb
|
| gptkbp:bfsParent |
gptkb:Supermarine_Spitfire_Mk.XVI
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Packard Merlin 266
|