gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:aircraft_operated
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gptkb:North_American_F-100_Super_Sabre
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gptkbp:application
|
gptkb:military_aircraft
|
gptkbp:average_temperature
|
1,500 ° F
|
gptkbp:check_in_time
|
optional
|
gptkbp:combustor_type
|
annular
|
gptkbp:compressor_type
|
axial
|
gptkbp:control_system
|
hydromechanical
|
gptkbp:cooling_system
|
air-cooled
|
gptkbp:design
|
gptkb:General_Electric
|
gptkbp:development
|
1950s
|
gptkbp:diameter
|
3 ft 4 in
|
gptkbp:emissions_standard
|
low
|
gptkbp:engine
|
modular
Brayton cycle
air start
J79 family
|
gptkbp:engine_configuration
|
gptkb:turbofan_engine
|
gptkbp:engine_power
|
2,500 hours
|
gptkbp:engine_type
|
open cycle
|
gptkbp:first_flight
|
gptkb:1955
|
gptkbp:fuel_economy
|
high
0.85 lb/lbf/hr
high at full throttle
|
gptkbp:fuel_type
|
JP-4
|
gptkbp:historical_significance
|
pioneering turbojet technology
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric J79-GE-21
|
gptkbp:influence
|
subsequent jet engine designs
|
gptkbp:introduced
|
gptkb:1955
|
gptkbp:invention
|
multiple patents filed
|
gptkbp:is_tested_for
|
extensive
|
gptkbp:legacy
|
widely used in 1960s aircraft
|
gptkbp:length
|
15 ft 9 in
|
gptkbp:maintenance
|
1,000 hours
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
gptkbp:marketed_as
|
limited
|
gptkbp:noise_level
|
moderate
|
gptkbp:notable_mission
|
strategic air power
|
gptkbp:notable_users
|
gptkb:F-16_Fighting_Falcon
|
gptkbp:number_of_engines
|
over 20,000
|
gptkbp:operational_history
|
extensive in military aviation
|
gptkbp:operational_range
|
1,000 miles
|
gptkbp:propulsion
|
not available
17,000 lbf
4.47
|
gptkbp:replaced_by
|
gptkb:F110_engine
|
gptkbp:research_and_development
|
ongoing improvements
|
gptkbp:retired
|
1990s
|
gptkbp:service_ceiling
|
50,000 ft
|
gptkbp:turbine_type
|
single spool
|
gptkbp:type
|
turbojet
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
|
gptkbp:variant
|
gptkb:J79-GE-15
|
gptkbp:weight
|
3,800 lb
|
gptkbp:bfsParent
|
gptkb:General_Electric_F101
|
gptkbp:bfsLayer
|
5
|