|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:F414_Engine
|
|
gptkbp:application
|
gptkb:battle
|
|
gptkbp:average_temperature
|
1,600 ° F
|
|
gptkbp:controls
|
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
36 inches
|
|
gptkbp:emissions_standard
|
Nox compliant
|
|
gptkbp:engine
|
gptkb:F414_family
twin-engine
6,000 hours
|
|
gptkbp:engine_type
|
axial
high bypass ratio
|
|
gptkbp:exported_to
|
gptkb:Australia
gptkb:Brazil
gptkb:India
gptkb:Kuwait
gptkb:Malaysia
gptkb:Qatar
gptkb:Saudi_Arabia
gptkb:Spain
gptkb:United_Arab_Emirates
gptkb:Native_American_tribe
|
|
gptkbp:features
|
modular design
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_capacity
|
high
|
|
gptkbp:fuel_type
|
gptkb:JP-5
gptkb:full_authority_digital_engine_control_(FADEC)
annular
|
|
gptkbp:has_programs
|
gptkb:F414_engine_program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F414-GE-400 X
|
|
gptkbp:length
|
160 inches
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 1.8
|
|
gptkbp:military_technology
|
gptkb:none
gptkb:battle
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_range
|
high altitude
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:propulsion
|
5.8
22,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
50,000 feet
|
|
gptkbp:successor
|
gptkb:F404_engine
|
|
gptkbp:type
|
afterburning turbofan engine
|
|
gptkbp:used_in
|
gptkb:F/_A-18_E/_F_Super_Hornet
|
|
gptkbp:weight
|
3,800 lb
|