|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:aircraft_type
|
attack aircraft engine
|
|
gptkbp:amended_by
|
revised for improved performance
|
|
gptkbp:application
|
close air support missions
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combat_experience
|
proven in combat experience
|
|
gptkbp:competitors
|
gptkb:General_Electric_F110
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:configuration
|
dual-spool
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:cooling_system
|
advanced cooling system
|
|
gptkbp:design
|
designed for durability
|
|
gptkbp:design_features
|
incorporates advanced design features
|
|
gptkbp:development
|
developed for the A-10 aircraft
|
|
gptkbp:diameter
|
approximately 3 ft 4 in
|
|
gptkbp:emissions_standard
|
low emissions
|
|
gptkbp:engine_type
|
afterburning turbofan
|
|
gptkbp:environmental_impact
|
designed to minimize environmental impact
|
|
gptkbp:features
|
features thrust vectoring capabilities
|
|
gptkbp:first_flight
|
gptkb:1976
|
|
gptkbp:fuel_economy
|
good fuel efficiency
low fuel consumption
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:future_prospects
|
future upgrades planned
|
|
gptkbp:has_limitations
|
limited operational limitations
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
TF34-100 A
|
|
gptkbp:is_tested_for
|
extensively tested before service entry
|
|
gptkbp:legacy
|
remains in service today
|
|
gptkbp:length
|
approximately 12 ft 6 in
|
|
gptkbp:maintenance
|
modular design for easy maintenance
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:modifications
|
modifications for specific missions
|
|
gptkbp:noise_level
|
low noise level
|
|
gptkbp:operational_history
|
used extensively in the Gulf War
|
|
gptkbp:operational_use
|
multi-role combat aircraft engine
|
|
gptkbp:part_of
|
gptkb:United_States_Air_Force_fleet
|
|
gptkbp:performance
|
excellent performance at low speeds
|
|
gptkbp:produces
|
produced in large numbers
|
|
gptkbp:propulsion
|
high thrust-to-weight ratio
around 9,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:Fairchild_Republic_A-10_Thunderbolt_II
|
|
gptkbp:reliability
|
high reliability
high reliability rating
|
|
gptkbp:service_entry
|
gptkb:1977
|
|
gptkbp:successor
|
gptkb:TF34-100_B
|
|
gptkbp:support
|
supported by extensive logistics
|
|
gptkbp:training
|
pilot training includes TF34 operations
|
|
gptkbp:turbine_type
|
two-stage high-pressure turbine
|
|
gptkbp:type
|
military aircraft engine
|
|
gptkbp:upgrades
|
upgraded versions available
|
|
gptkbp:used_in
|
gptkb:A-10_Thunderbolt_II
|
|
gptkbp:weight
|
approximately 2,800 lb
|
|
gptkbp:bfsParent
|
gptkb:A-10_Thunderbolt_II
gptkb:A-10_Warthog
|
|
gptkbp:bfsLayer
|
4
|