Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:air_support |
1,200 lb/s
|
| gptkbp:compressor_type |
gptkb:9
|
| gptkbp:design |
twin-spool
|
| gptkbp:diameter |
1.1 m
|
| gptkbp:engine_configuration |
high bypass ratio
|
| gptkbp:first_flight |
gptkb:1986
|
| gptkbp:fuel_economy |
0.5 lb/lbf/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric F118
|
| gptkbp:length |
3.8 m
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:propulsion |
22,000 lbf
|
| gptkbp:turbine_type |
2
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:Mc_Donnell_Douglas_F-18_Hornet
gptkb:Mc_Donnell_Douglas_F-15_Eagle |
| gptkbp:weight |
1,200 kg
|
| gptkbp:bfsParent |
gptkb:General_Electric_F101
|
| gptkbp:bfsLayer |
5
|