Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turboprop engine
|
| gptkbp:application |
military transport aircraft
|
| gptkbp:compressionRatio |
12:1
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:developer |
developed from the T56 engine family.
|
| gptkbp:diameter |
1,200 mm
|
| gptkbp:engineType |
4
turboprop |
| gptkbp:firstFlight |
1954
|
| gptkbp:fuel_capacity |
0.5 lb/hp/hr
|
| gptkbp:fuelType |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce T56-A-15
|
| gptkbp:is_used_in |
gptkb:Lockheed_C-130_Hercules
|
| gptkbp:length |
1,800 mm
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notable_feature |
T56-A-15A
|
| gptkbp:operationalHistory |
used in various military and civilian aircraft.
|
| gptkbp:powerOutput |
4,600 shp
|
| gptkbp:propulsion |
5,000 lbf
|
| gptkbp:related_engine |
gptkb:Pratt_&_Whitney_PT6
|
| gptkbp:service_ceiling |
25,000 ft
|
| gptkbp:setting |
twin-shaft
|
| gptkbp:weight |
1,200 kg
|