Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:aircraft_operated |
gptkb:Lockheed_L-1011_Tri_Star
gptkb:Airbus gptkb:Mc_Donnell_Douglas_DC-10 |
| gptkbp:application |
commercial aviation
|
| gptkbp:bypass_ratio |
5.5:1
|
| gptkbp:compressor_type |
axial
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
3.0 ft
96 in |
| gptkbp:engine_configuration |
twin-spool
|
| gptkbp:first_flight |
gptkb:1970
|
| gptkbp:fuel_economy |
0.5 lb/lbf/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
CF6-50 C12
|
| gptkbp:length |
12.5 ft
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:propulsion |
50,000 lbf
|
| gptkbp:turbine_type |
high bypass ratio
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:weight |
4,000 lb
|
| gptkbp:bfsParent |
gptkb:CF6-50_C
|
| gptkbp:bfsLayer |
7
|