|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
civilian aircraft
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial-flow
|
|
gptkbp:control_system
|
hydromechanical fuel control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:development
|
gptkb:J79-GE-15
gptkb:J79-GE-5
|
|
gptkbp:diameter
|
approximately 3 ft 4 in
|
|
gptkbp:engine
|
air-start
widely used in the 1960s and 1970s
1950s technology
|
|
gptkbp:engine_power
|
high reliability
moderate efficiency
|
|
gptkbp:engine_power_to_weight_ratio
|
high power-to-weight ratio
|
|
gptkbp:engine_type
|
gptkb:J79-GE-11
gptkb:J79-GE-15
gptkb:J79-GE-19
gptkb:J79-GE-17
gptkb:J79-GE-20
gptkb:J79-GE-21
gptkb:J79-GE-22
gptkb:J79-GE-24
gptkb:J79-GE-25
gptkb:J79-GE-26
gptkb:J79-GE-27
gptkb:J79-GE-28
gptkb:J79-GE-30
gptkb:J79-GE-5
gptkb:J79-GE-8
J79-GE-23
J79-GE-29
|
|
gptkbp:first_flight
|
gptkb:1955
|
|
gptkbp:fuel_type
|
JP-4
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric J79
|
|
gptkbp:length
|
approximately 15 ft 9 in
|
|
gptkbp:maintenance
|
modular design
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
high noise level
|
|
gptkbp:notable_users
|
gptkb:Israeli_Air_Force
gptkb:Royal_Canadian_Air_Force
gptkb:United_States_Air_Force
gptkb:United_States_Navy
gptkb:Turkish_Air_Force
|
|
gptkbp:propulsion
|
no
around 15,000 lbf
|
|
gptkbp:replaced_by
|
gptkb:F110_engine
|
|
gptkbp:retirement_year
|
1990s
|
|
gptkbp:service_entry
|
gptkb:1956
|
|
gptkbp:turbine_type
|
single-stage high-pressure turbine
|
|
gptkbp:type
|
afterburning turbojet
|
|
gptkbp:used_in
|
gptkb:F-16_Fighting_Falcon
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
|
|
gptkbp:variant
|
gptkb:J79-GE-17
gptkb:J79-GE-8
|
|
gptkbp:weight
|
approximately 2,500 lb
|
|
gptkbp:bfsParent
|
gptkb:F-4_Phantom_II
gptkb:F-16_Fighting_Falcon
|
|
gptkbp:bfsLayer
|
4
|