Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:combustor_type |
annular
|
| gptkbp:compressor_type |
axial
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
36 in
|
| gptkbp:first_flight |
gptkb:1999
|
| 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 H
|
| gptkbp:length |
160 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:propulsion |
22,000 lbf
|
| gptkbp:service_ceiling |
50,000 ft
|
| gptkbp:successor |
F404-GE-400
|
| gptkbp:turbine_type |
high bypass ratio
|
| gptkbp:type |
afterburning turbofan
|
| 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
|