Statements (26)
| 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:diameter |
2.5 ft
|
| gptkbp:emissionsStandard |
low
|
| gptkbp:energyEfficiency |
high
|
| gptkbp:firstFlight |
1954
|
| gptkbp:fuelType |
Jet_fuel
|
| https://www.w3.org/2000/01/rdf-schema#label |
T56-A-427 turboprop
|
| gptkbp:length |
4.5 ft
|
| gptkbp:maintenance |
1,500 hours
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:noise_level |
low
|
| gptkbp:numberOfEpisodes |
4
|
| gptkbp:operationalRange |
1,500 miles
|
| gptkbp:powerOutput |
4,600 shp
|
| gptkbp:propulsion |
constant-speed propeller
4,600 lbf |
| gptkbp:related_engine |
Brayton_cycle
|
| gptkbp:reliability |
high
|
| gptkbp:setting |
twin-shaft
|
| gptkbp:type |
turbo-prop engine
|
| gptkbp:usedIn |
gptkb:Lockheed_C-130_Hercules
|
| gptkbp:weight |
1,200 lb
|