|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:certification
|
military certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
hydromechanical
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:emissions_standard
|
high
|
|
gptkbp:engine
|
gptkb:fighter_aircraft
Brayton cycle
air start
produced in large numbers
used in various aircraft types
upgraded over time
J79 family
|
|
gptkbp:engine_configuration
|
gptkb:J79-GE-19
inline
single spool
turbojet design
|
|
gptkbp:engine_influence
|
influenced future jet engine designs
|
|
gptkbp:engine_power
|
high performance
reliable
retired from service
|
|
gptkbp:first_flight
|
gptkb:1958
|
|
gptkbp:fuel_economy
|
moderate
0.85 lb/hp/hr
|
|
gptkbp:fuel_type
|
JP-4
|
|
gptkbp:history
|
developed in the 1950s
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric J79-GE-19
|
|
gptkbp:intended_use
|
gptkb:military_aircraft
|
|
gptkbp:is_tested_for
|
extensively tested
|
|
gptkbp:length
|
15 ft 9 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 2.2
|
|
gptkbp:noise_level
|
high
|
|
gptkbp:number_of_rooms
|
can-type
|
|
gptkbp:operational_use
|
gptkb:Vietnam_War
|
|
gptkbp:propulsion
|
no
17,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:F-4_Phantom_family
|
|
gptkbp:replaced_by
|
gptkb:F110_engine
|
|
gptkbp:service_history
|
used in military aircraft
|
|
gptkbp:turbine_type
|
axial
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
|
|
gptkbp:variant
|
gptkb:J79-GE-15
gptkb:J79-GE-17
gptkb:J79-GE-21
|
|
gptkbp:weight
|
3,800 lb
|
|
gptkbp:bfsParent
|
gptkb:General_Electric_F101
|
|
gptkbp:bfsLayer
|
5
|