Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
6
|
| gptkbp:bfsParent |
gptkb:F414-GE-400_X
|
| gptkbp:aircraft_operated |
gptkb:F/_A-18_family
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:diameter |
3 ft 4 in
|
| gptkbp:engine |
twin-spool
|
| gptkbp:engine_type |
axial compressor
two-stage high-pressure turbine |
| gptkbp:fan_art |
single-stage fan
|
| gptkbp:first_flight |
gptkb:1995
|
| gptkbp:fuel_type |
gptkb:JP-5
annular combustor |
| https://www.w3.org/2000/01/rdf-schema#label |
F414 family
|
| gptkbp:length |
12 ft 6 in
|
| gptkbp:produced_by |
gptkb:General_Electric
|
| gptkbp:propulsion |
22,000 lbf
|
| gptkbp:successor |
F404 family
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:used_in |
gptkb:Boeing_F/_A-18_E/_F_Super_Hornet
gptkb:Mc_Donnell_Douglas_F/_A-18_Hornet |
| gptkbp:weight |
1,500 lb
|