Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:transport_aircraft
|
| gptkbp:compression_ratio |
12:1
|
| gptkbp:configuration |
twin-shaft
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
2.5 ft
|
| gptkbp:engine |
Brayton cycle
|
| gptkbp:engine_type |
turboprop
|
| gptkbp:first_flight |
gptkb:1954
|
| gptkbp:fuel_economy |
0.5 lb/hp/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison T56-A-15
|
| gptkbp:length |
4.5 ft
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:number_of_engines |
gptkb:4
|
| gptkbp:power_output |
4,600 shp
|
| gptkbp:propeller |
gptkb:Hamilton_Standard_54_H60-77
|
| gptkbp:type |
turbo-prop engine
|
| gptkbp:used_in |
gptkb:Lockheed_C-130_Hercules
|
| gptkbp:weight |
1,200 lb
1,800 lb |
| gptkbp:bfsParent |
gptkb:Hercules_X-11
|
| gptkbp:bfsLayer |
5
|