Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
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 cubic inches
|
| gptkbp:firstFlight |
1942
|
| gptkbp:fuelType |
100-octane aviation gasoline
|
| gptkbp:height |
40 in
|
| https://www.w3.org/2000/01/rdf-schema#label |
Packard V-1650-1 Merlin
|
| gptkbp:length |
88.25 in
|
| gptkbp:manufacturer |
gptkb:Packard
|
| gptkbp:notableFor |
enabled high-altitude performance in P-51 Mustang
|
| gptkbp:powerOutput |
1,300 hp
|
| gptkbp:productionStartYear |
1941-1945
|
| gptkbp:stroke |
6.0 in
|
| gptkbp:supercharger |
single-stage, two-speed
|
| gptkbp:usedInAircraft |
gptkb:aircraft
gptkb:Curtiss_P-40F Avro Lancaster (some variants) |
| gptkbp:valvetrain |
DOHC, 4 valves per cylinder
|
| gptkbp:weight |
1,640 lb (dry)
|
| gptkbp:width |
30.13 in
|
| gptkbp:bfsParent |
gptkb:Curtiss_P-40L
|
| gptkbp:bfsLayer |
8
|