|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
fighter jets
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
mechanical
|
|
gptkbp:cooling_system
|
air-cooled
used for turbine cooling
|
|
gptkbp:design_features
|
afterburner
|
|
gptkbp:development
|
1950s
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:emissions_standard
|
moderate
|
|
gptkbp:engine
|
Brayton cycle
air start
upgraded versions available
mass produced
|
|
gptkbp:engine_configuration
|
modular design
inline
single engine
|
|
gptkbp:engine_power
|
high speed performance
|
|
gptkbp:first_flight
|
gptkb:1958
|
|
gptkbp:fuel_economy
|
moderate
high at full throttle
|
|
gptkbp:fuel_type
|
JP-4
|
|
gptkbp:historical_significance
|
pioneering jet engine technology
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric J79-GE-17
|
|
gptkbp:is_tested_for
|
static testing
|
|
gptkbp:legacy
|
influenced future jet engine designs
|
|
gptkbp:length
|
15 ft 9 in
|
|
gptkbp:maintenance
|
short
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
high
|
|
gptkbp:operational_range
|
high speed
|
|
gptkbp:operational_use
|
gptkb:Vietnam_War
|
|
gptkbp:propulsion
|
4.5:1
17,000 lbf
|
|
gptkbp:related_aircraft
|
naval aircraft
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_history
|
used in military aircraft
|
|
gptkbp:successor
|
gptkb:General_Electric_F404
|
|
gptkbp:turbine_type
|
single spool
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
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
|