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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:aircraft_operated
|
gptkb:Grumman_F-14_Tomcat
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:compression_ratio
|
25:1
|
|
gptkbp:controls
|
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
gptkb:engine
|
|
gptkbp:diameter
|
2.5 ft
|
|
gptkbp:emissions_standard
|
low emissions
mixed-flow exhaust
variable geometry air intake
|
|
gptkbp:engine
|
gptkb:F404/_F414_family
Brayton cycle
3,000 hours
twin-spool configuration
|
|
gptkbp:exported_to
|
several countries
|
|
gptkbp:fan_art
|
single-stage fan
|
|
gptkbp:fighting_style
|
gptkb:battle
|
|
gptkbp:first_flight
|
gptkb:1983
|
|
gptkbp:fuel_capacity
|
high efficiency
0.85 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:JP-5
annular combustor
hydromechanical fuel control
|
|
gptkbp:has_programs
|
Y F404
|
|
gptkbp:has_variants
|
multiple variants
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F404 engine
|
|
gptkbp:is_tested_for
|
extensive testing conducted
|
|
gptkbp:length
|
4.5 ft
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_feature
|
afterburner capability
|
|
gptkbp:operated_by
|
multiple air forces
|
|
gptkbp:operational_area
|
gptkb:aircraft
gptkb:1984
|
|
gptkbp:operational_range
|
long operational range
|
|
gptkbp:part_of
|
gptkb:aircraft
|
|
gptkbp:power_output
|
16,000 to 22,000 lbf
|
|
gptkbp:propulsion
|
22,000 lbf
no thrust vectoring
18.3:1
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:successor
|
gptkb:F414_engine
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F/_A-18_Hornet
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:F414_engine
|
|
gptkbp:bfsLayer
|
5
|