|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:F414_Engine
gptkb:F414_engine
gptkb:General_Electric_F414
gptkb:Pratt_&_Whitney_F414
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
36 in
|
|
gptkbp:engine
|
gptkb:F414-GE-400
gptkb:F/_A-18_E/_F_Super_Hornet
high
good
possible
ongoing
excellent
widely available
twin-spool
air start
developed from F404 engine.
|
|
gptkbp:engine_type
|
gptkb:F414-GE-400_E-400
axial compressor
high-pressure turbine
|
|
gptkbp:fan_art
|
single-stage fan
|
|
gptkbp:first_flight
|
gptkb:1999
|
|
gptkbp:fuel_capacity
|
4.1 m
0.8 lb/lbf/hr
1,360 kg
0.91 m
|
|
gptkbp:fuel_type
|
gptkb:JP-5
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F414-GE-400 E
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:length
|
160 in
|
|
gptkbp:maintenance
|
modular design
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:military_branch
|
gptkb:battle
|
|
gptkbp:noise_level
|
low
moderate
|
|
gptkbp:number_of_stages
|
gptkb:9
|
|
gptkbp:propulsion
|
gptkb:battle
22,000 lbf
13,000 lbf
7.5 lbf/lb
|
|
gptkbp:services
|
gptkb:2001
|
|
gptkbp:successor
|
F404-GE-400
|
|
gptkbp:type
|
afterburning turbofan engine
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F/_A-18_Hornet
|
|
gptkbp:variant
|
gptkb:F414-GE-400_E-400
|
|
gptkbp:weight
|
3,000 lb
|