|
gptkbp:instanceOf
|
turboprop engine
|
|
gptkbp:application
|
military aircraft
civil aircraft
|
|
gptkbp:certifications
|
FAA_certified
|
|
gptkbp:climate
|
high
|
|
gptkbp:compressionRatio
|
16:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
modular
|
|
gptkbp:developer
|
1950s
|
|
gptkbp:diameter
|
2.5 ft
|
|
gptkbp:emissionsStandard
|
low
|
|
gptkbp:engineConfiguration
|
twin-shaft
|
|
gptkbp:engineType
|
4
free turbine
axial compressor
|
|
gptkbp:firstFlight
|
1954
|
|
gptkbp:fuel_capacity
|
high
0.5 lb/hp/hr
|
|
gptkbp:fuelType
|
Jet A
annular
spark ignition
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Allison T56-A-9
|
|
gptkbp:is_used_in
|
gptkb:Lockheed_C-130_Hercules
gptkb:Lockheed_P-3_Orion
|
|
gptkbp:landing_gear
|
16:1
|
|
gptkbp:legal_principle
|
turbine engine
|
|
gptkbp:length
|
4.5 ft
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Allison_Engine_Company
|
|
gptkbp:market
|
global
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:number_of_stages
|
14
|
|
gptkbp:operationalRange
|
1,500 miles
|
|
gptkbp:performances
|
5,000 hours
|
|
gptkbp:powerOutput
|
1,600 to 4,600 shp
|
|
gptkbp:propulsion
|
gptkb:Hamilton_Standard_54H60-77
3,000 lb
|
|
gptkbp:related_engine
|
gptkb:Pratt_&_Whitney_PT6
gptkb:Rolls-Royce_AE_3007
gptkb:General_Electric_T64
Brayton_cycle
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:successor
|
gptkb:Allison_T56-A-15
|
|
gptkbp:type
|
turbo-prop engine
|
|
gptkbp:weight
|
1,200 lb
|