Statements (23)
| 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:diameter |
29.25 in
|
| gptkbp:displacement |
1650 cubic inches
|
| gptkbp:firstFlight |
1942
|
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Packard V-1650-9 Merlin
|
| gptkbp:length |
88.25 in
|
| gptkbp:manufacturer |
gptkb:Packard
|
| gptkbp:powerOutput |
about 1,720 hp
|
| gptkbp:stroke |
6.0 in
|
| gptkbp:supercharger |
two-stage
|
| gptkbp:usedDuring |
gptkb:World_War_II
|
| gptkbp:usedIn |
gptkb:aircraft
gptkb:Curtiss_P-40Q |
| gptkbp:weight |
1,640 lb
|
| gptkbp:bfsParent |
gptkb:P-51H
|
| gptkbp:bfsLayer |
6
|