Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| 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 |
2.5 m
3.0 ft |
| gptkbp:emissions_standard |
Stage 3
|
| gptkbp:engine_configuration |
twin-spool
|
| gptkbp:first_flight |
gptkb:1971
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
CF6-50
|
| gptkbp:length |
12.5 ft
|
| gptkbp:maintenance |
6,000 hours
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:noise_level |
low noise
|
| gptkbp:notable_users |
gptkb:Airbus
gptkb:Mc_Donnell_Douglas_DC-10 |
| gptkbp:operational_range |
up to 8,000 miles
|
| gptkbp:propulsion |
50,000 lbf
|
| gptkbp:successor |
gptkb:CF6-80
|
| gptkbp:turbine_type |
high bypass turbofan
|
| gptkbp:weight |
4,000 lb
|
| gptkbp:bfsParent |
gptkb:E-4_B_Nightwatch
gptkb:Airbus gptkb:Sentry |
| gptkbp:bfsLayer |
4
|