|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_type
|
gptkb:fighter_aircraft
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:check_in_time
|
optional
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
hydromechanical
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:development
|
gptkb:General_Electric
|
|
gptkbp:diameter
|
30 in
|
|
gptkbp:emissions_standard
|
compliant with regulations
|
|
gptkbp:engine
|
Brayton cycle
air start
J85-GE-17
|
|
gptkbp:engine_configuration
|
turbojet
pylon-mounted
single engine
|
|
gptkbp:engine_power
|
3,000 hours
|
|
gptkbp:engine_type
|
turbojet
|
|
gptkbp:first_flight
|
gptkb:1956
|
|
gptkbp:fuel_economy
|
high
0.85 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric J85-GE-23
|
|
gptkbp:ignition_system
|
gptkb:spark_plug
|
|
gptkbp:length
|
12.5 in
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 2.2
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_history
|
used by various air forces
|
|
gptkbp:operational_use
|
gptkb:trainer_aircraft
|
|
gptkbp:origin
|
gptkb:USA
|
|
gptkbp:power_output
|
5,000 hp
|
|
gptkbp:propulsion
|
3,850 lbf
6.42
|
|
gptkbp:related_aircraft
|
gptkb:Northrop_F-5
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:turbine_type
|
single spool
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
|
|
gptkbp:variant
|
J85-GE-21
|
|
gptkbp:water_requirement
|
300 lb/hr
|
|
gptkbp:weight
|
600 lb
|
|
gptkbp:bfsParent
|
gptkb:General_Electric_F101
|
|
gptkbp:bfsLayer
|
5
|