Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:aircraft_operated |
gptkb:aircraft
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:developer |
gptkb:General_Electric
|
| gptkbp:diameter |
3 ft 4 in
8 ft 4 in |
| gptkbp:engine |
gptkb:General_Electric_F110
Brayton cycle twin-spool |
| gptkbp:engine_type |
axial
high bypass ratio |
| gptkbp:first_flight |
gptkb:1986
|
| gptkbp:fuel_capacity |
0.5 lb/lbf/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric F118-101
|
| gptkbp:length |
12 ft 6 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notable_features |
reheat capability
|
| gptkbp:operational_area |
gptkb:aircraft
|
| gptkbp:propulsion |
29,000 lbf
|
| gptkbp:services |
gptkb:1990
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:Mc_Donnell_Douglas_F-15_Eagle
|
| gptkbp:weight |
3,000 lb
|
| gptkbp:bfsParent |
gptkb:U._S._U-2_spy_plane
|
| gptkbp:bfsLayer |
5
|