Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:compressor_type |
axial
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
3 ft 9 in
|
| gptkbp:first_flight |
gptkb:1971
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
CF6-50 S
|
| gptkbp:length |
12 ft 6 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notable_users |
gptkb:Airbus
gptkb:Mc_Donnell_Douglas_DC-10 |
| gptkbp:propulsion |
50,000 lbf
|
| gptkbp:successor |
CF6-80 C2
|
| gptkbp:turbine_type |
high bypass ratio
|
| gptkbp:weight |
3,000 lb
|
| gptkbp:bfsParent |
gptkb:General_Electric_CF6-50
|
| gptkbp:bfsLayer |
6
|