Lycoming T53

GPTKB entity

Statements (66)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application gptkb:Sikorsky_CH-54_Tarhe
gptkb:Boeing_CH-47_Chinook
gptkb:Bell_UH-1_Iroquois
gptkbp:armament 2
gptkbp:average_temperature up to 1,000 ° F
gptkbp:compression_ratio 8:1
gptkbp:control_system hydromechanical fuel control
gptkbp:cooling_system air-cooled
gptkbp:design turbo-shaft
gptkbp:development developed for military use
gptkbp:emissions_standard low emissions
gptkbp:engine turbo-shaft engine class
gptkbp:engine_configuration single-shaft
T53-L-13
T53-L-701
T53-L-11
T53-L-703
T53-L-1
T53-L-10
T53-L-12
T53-L-14
T53-L-15
T53-L-16
T53-L-17
T53-L-18
T53-L-19
T53-L-2
T53-L-20
T53-L-3
T53-L-4
T53-L-5
T53-L-6
T53-L-7
T53-L-8
T53-L-9
gptkbp:first_flight 1950s
gptkbp:fuel_economy 0.5 lb/hp/hr
gptkbp:fuel_type aviation kerosene
gptkbp:gearbox reduction gearbox
https://www.w3.org/2000/01/rdf-schema#label Lycoming T53
gptkbp:ignition_system dual ignition
gptkbp:maintenance 500 hours
gptkbp:manufacturer gptkb:Lycoming_Engines
gptkbp:market gptkb:military_aircraft
gptkbp:noise_level moderate noise
gptkbp:operational_range up to 30,000 feet
gptkbp:power_output 1,500 to 1,800 shp
gptkbp:propulsion 5:1
gptkbp:reliability high reliability
gptkbp:service up to 5,000 hours
gptkbp:successor gptkb:Lycoming_T55
gptkbp:turbine_type free turbine
gptkbp:type gptkb:turbofan_engine
gptkbp:used_in gptkb:helicopter
gptkbp:weight approximately 300 lbs
gptkbp:bfsParent gptkb:Bell_AH-1_Cobra
gptkb:AH-1_Cobra_helicopter
gptkb:Bell_UH-1_D
gptkb:Bell_UH-1_Iroquois
gptkb:AH-1_Cobra
gptkb:Huey_helicopter
gptkb:OV-10_Bronco
gptkb:UH-1_Huey
gptkb:UH-1_Iroquois
gptkbp:bfsLayer 5