gptkbp:instance_of
|
gptkb:jet_engine
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gptkbp:application
|
gptkb:military_aircraft
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gptkbp:average_temperature
|
1,500 ° F.
1,600 ° F.
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gptkbp:check_in_time
|
yes.
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gptkbp:combustor_type
|
annular
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gptkbp:compressor_type
|
axial
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gptkbp:control_system
|
hydromechanical.
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gptkbp:cooling_system
|
air-cooled.
intercooling.
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gptkbp:design
|
gptkb:General_Electric
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gptkbp:design_features
|
high thrust-to-weight ratio.
|
gptkbp:development
|
1950s.
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gptkbp:diameter
|
3 ft 4 in
|
gptkbp:emissions_standard
|
military standards.
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gptkbp:engine
|
influenced future designs.
advanced for its time.
developed in the 1950s.
limited production.
modular.
Brayton cycle.
significant in jet engine development.
General Electric J79.
J-series.
air start.
military aviation market.
operational in the 1960s.
various military aircraft.
|
gptkbp:engine_configuration
|
detailed specifications available.
performance-oriented.
turbojet.
characteristics include high thrust.
single-spool.
|
gptkbp:engine_power
|
high performance.
high reliability.
3,000 hours.
moderate efficiency.
retired in the 1970s.
|
gptkbp:engine_production_year
|
1958.
|
gptkbp:engine_type
|
J93-GE-3.
|
gptkbp:first_flight
|
gptkb:1958
|
gptkbp:fuel_economy
|
0.8 lb/hp/hr.
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric J93-GE-3
|
gptkbp:ignition_system
|
spark plug.
|
gptkbp:is_tested_for
|
General Electric facilities.
static and flight tests.
|
gptkbp:length
|
15 ft 6 in
|
gptkbp:maintenance
|
1,000 hours.
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
gptkbp:max_speed
|
Mach 2.2.
|
gptkbp:noise_level
|
high.
|
gptkbp:notable_users
|
U. S. Air Force.
|
gptkbp:number_of_engines
|
two.
|
gptkbp:operational_history
|
used in various military applications.
|
gptkbp:predecessor
|
gptkb:General_Electric_J85
|
gptkbp:propulsion
|
15,000 lbf
no.
5.36.
|
gptkbp:service_ceiling
|
50,000 ft.
|
gptkbp:successor
|
gptkb:General_Electric_J79
|
gptkbp:turbine_type
|
single spool
|
gptkbp:type
|
gptkb:turbofan_engine
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
|
gptkbp:weight
|
2,800 lb
|
gptkbp:bfsParent
|
gptkb:General_Electric_F101
|
gptkbp:bfsLayer
|
5
|