T58-GE-10 turboshaft

GPTKB entity

Statements (54)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:bfsLayer 5
gptkbp:bfsParent gptkb:RH-53_Sea_Stallion
gptkb:SH-3_Sea_King
gptkbp:application gptkb:helicopter
gptkbp:average_temperature high turbine inlet temperature
up to 1,000 ° F
gptkbp:controls hydromechanical control
gptkbp:cooling_system air-cooled
air cooling
gptkbp:diameter approximately 14 in
gptkbp:drivetrain reduction gearbox
gptkbp:emissions_standard low emissions
gptkbp:engine gptkb:T58-GE-400
twin-spool
horizontal layout
up to 5,000 hours
gptkbp:engine_type axial compressor
single-stage turbine
gptkbp:environmental_impact low environmental impact
gptkbp:features modular design
gptkbp:first_flight gptkb:1956
gptkbp:fuel_capacity good fuel efficiency
approximately 0.5 lb/hp/hr
gptkbp:fuel_type gptkb:Company
gptkb:Jet_A
gptkbp:historical_event developed in the 1950s
gptkbp:historical_significance significant in military aviation history
https://www.w3.org/2000/01/rdf-schema#label T58-GE-10 turboshaft
gptkbp:ignition_system spark ignition
gptkbp:is_tested_for extensively tested
gptkbp:launch_site starter-generator
gptkbp:legacy influenced future turboshaft designs
gptkbp:legal_issue Brayton cycle
gptkbp:length approximately 40 in
gptkbp:maintenance 1,000 hours
gptkbp:manufacturer gptkb:General_Electric
gptkbp:market_segment gptkb:aircraft
gptkbp:material aluminum alloys
gptkbp:noise_level moderate noise level
gptkbp:notable_features high power-to-weight ratio
gptkbp:notable_users gptkb:military_unit
gptkbp:operational_area widely used in helicopters
gptkbp:power_output 1,400 shp
gptkbp:propulsion 3.5:1
3.5 hp/lb
gptkbp:regulatory_compliance FAA certified
gptkbp:reliability high reliability
gptkbp:service_ceiling up to 20,000 ft
gptkbp:successor gptkb:T700_engine
gptkbp:type gptkb:engine
gptkbp:used_in gptkb:Bell_UH-1_Iroquois
gptkbp:variant T58-GE-8
gptkbp:weight approximately 400 lb