Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
5.4 in
|
| gptkbp:compressionRatio |
6.0:1
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:designer |
gptkb:Rolls-Royce
|
| gptkbp:displacement |
1,649 cubic inches
|
| gptkbp:engineType |
V-12 piston engine
|
| gptkbp:firstProduced |
1943
|
| gptkbp:fuelType |
aviation gasoline
carburetor |
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Merlin V-1650-9
|
| gptkbp:manufacturer |
gptkb:Packard
|
| gptkbp:notableFeature |
improved high-altitude performance
|
| gptkbp:powerOutput |
1,720 hp
|
| gptkbp:stroke |
6.0 in
|
| gptkbp:supercharger |
two-stage, two-speed
|
| gptkbp:usedInAircraft |
gptkb:aircraft
gptkb:Curtiss_P-40 |
| gptkbp:valvetrain |
single overhead camshaft
|
| gptkbp:weight |
1,640 lb
|
| gptkbp:bfsParent |
gptkb:P-51H_Mustang
|
| gptkbp:bfsLayer |
6
|