Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:basedOn |
gptkb:Rolls-Royce_Merlin
|
| gptkbp:bore |
5.4 in
|
| gptkbp:compressionRatio |
6.0:1
|
| gptkbp:configuration |
liquid-cooled
|
| gptkbp:coolingSystem |
gptkb:water
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:displacement |
1,649 cubic inches
|
| gptkbp:engineType |
V12
|
| gptkbp:firstFlight |
1942
|
| gptkbp:fuelType |
100/130 octane aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Packard V-1650-7 Merlin V12
|
| gptkbp:manufacturer |
gptkb:Packard
|
| gptkbp:notableFeature |
improved high-altitude performance
licensed production of Rolls-Royce Merlin |
| gptkbp:powerOutput |
1,695 hp
|
| gptkbp:rpm |
3,000 rpm max
|
| gptkbp:stroke |
6.0 in
|
| gptkbp:supercharger |
two-stage, two-speed
|
| gptkbp:usedIn |
gptkb:aircraft
gptkb:Curtiss_P-40Q |
| gptkbp:valvetrain |
single overhead camshaft per bank
|
| gptkbp:weight |
1,640 lb dry
|
| gptkbp:bfsParent |
gptkb:aircraft
|
| gptkbp:bfsLayer |
4
|