Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:aircraft_operated |
gptkb:Boeing_707
gptkb:Airbus gptkb:Mc_Donnell_Douglas_MD-11 |
| gptkbp:application |
commercial aviation
|
| gptkbp:bypass_ratio |
8.5:1
|
| gptkbp:certification |
NOx
|
| gptkbp:compressor_type |
axial
|
| gptkbp:diameter |
3.0 ft
2.9 ft |
| gptkbp:engine |
Brayton cycle
|
| gptkbp:first_flight |
gptkb:1982
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
CF6-80 C2 B1 F1
|
| gptkbp:introduced |
gptkb:1982
|
| gptkbp:length |
11.5 ft
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:noise_level |
Stage 3
|
| gptkbp:number_of_stages |
gptkb:10
|
| gptkbp:propulsion |
60,000 lbf
|
| gptkbp:successor |
CF6-80 C2 B1 F2
|
| gptkbp:weight |
4,000 lb
|
| gptkbp:bfsParent |
gptkb:CF6
|
| gptkbp:bfsLayer |
5
|