Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:compressionRatio |
14-stage axial flow
|
| gptkbp:configuration |
single-shaft
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:firstFlight |
1954
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison T56-A-7 turboprop
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:partOf |
Allison T56 engine family
|
| gptkbp:powerOutput |
4,200 shp
|
| gptkbp:status |
in service
|
| gptkbp:usedIn |
gptkb:Lockheed_C-130_Hercules
gptkb:Lockheed_P-3_Orion |
| gptkbp:bfsParent |
gptkb:C-130E
gptkb:Lockheed_C-130B_Hercules gptkb:C-130B |
| gptkbp:bfsLayer |
7
|