gptkbp:instance_of
|
gptkb:engine
|
gptkbp:bfsLayer
|
5
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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
|