|
gptkbp:instanceOf
|
turboprop engine
|
|
gptkbp:application
|
military aircraft
maritime patrol aircraft
cargo_aircraft
|
|
gptkbp:compressionRatio
|
12:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:diameter
|
3.5 ft
|
|
gptkbp:engine
|
military and civilian aircraft
air-cooled
Jet A
1,800 lb
4.5 ft
pylon-mounted
air-start
|
|
gptkbp:engineConfiguration
|
free turbine
wet sump
twin-shaft
twin-shaft engine
|
|
gptkbp:engineDisplacement
|
3.5 ft
|
|
gptkbp:enginePower
|
4,600 shp
|
|
gptkbp:engineType
|
turbine engine
turboprop engine
T56-A-15
T56-A-16
T56-A-427
|
|
gptkbp:exhaustSystem
|
straight exhaust
|
|
gptkbp:firstFlight
|
1954
|
|
gptkbp:fuelCapacity
|
0.5 lb/hp/hr
|
|
gptkbp:fuelType
|
Jet A
annular combustion chamber
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Allison T56-A-427 turboprop
|
|
gptkbp:length
|
4.5 ft
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Allison_Engine_Company
|
|
gptkbp:maxSpeed
|
350 knots
|
|
gptkbp:numberOfEpisodes
|
4
|
|
gptkbp:operationalHistory
|
developed in the 1950s
|
|
gptkbp:powerOutput
|
4,600 shp
|
|
gptkbp:propulsion
|
2.56
variable-pitch propeller
2.56 hp/lb
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:services
|
25,000 ft
|
|
gptkbp:type
|
turbo-prop engine
|
|
gptkbp:usedIn
|
gptkb:Lockheed_C-130_Hercules
gptkb:Lockheed_P-3_Orion
|
|
gptkbp:weight
|
1,800 lb
|