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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
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gptkb:military_aircraft
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|
gptkbp:average_temperature
|
1,600 ° F
|
|
gptkbp:certification
|
military certification
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|
gptkbp:combustor_type
|
annular combustor
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|
gptkbp:compressor_type
|
axial compressor
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|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
36 in
|
|
gptkbp:engine
|
gptkb:military_aircraft
gptkb:F414-GE-400
global support network
air start
produced in large quantities
collaboration with military branches
developed from F404 engine technology
part of the F414 family of engines.
upgradable for future enhancements
|
|
gptkbp:engine_configuration
|
twin-spool
twin-spool turbofan
|
|
gptkbp:engine_power
|
high performance
high reliability
|
|
gptkbp:engine_type
|
gptkb:F414-GE-400_E
turbofan
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_capacity
|
4.1 m
1,588 kg
0.91 m
|
|
gptkbp:fuel_economy
|
0.8 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:JP-5
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F414-GE-400 Z
|
|
gptkbp:is_tested_for
|
extensive ground testing
|
|
gptkbp:length
|
160 in
|
|
gptkbp:maintenance
|
modular design for easy maintenance
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 1.8
|
|
gptkbp:noise_level
|
low noise emissions
|
|
gptkbp:notable_features
|
reduced maintenance costs
|
|
gptkbp:operational_range
|
1,250 nautical miles
|
|
gptkbp:propulsion
|
22,000 lbf
6.3:1
|
|
gptkbp:reheat_thrust
|
26,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:F/_A-18_Super_Hornet
|
|
gptkbp:service_entry
|
gptkb:1999
|
|
gptkbp:successor
|
gptkb:F404_engine
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:type
|
afterburning turbofan engine
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F/_A-18_Hornet
|
|
gptkbp:weight
|
3,500 lb
|
|
gptkbp:bfsParent
|
gptkb:General_Electric_F414_engine
|
|
gptkbp:bfsLayer
|
8
|