Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Dart
|
| gptkbp:application |
commercial aviation
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
1.8 m
|
| gptkbp:engine_type |
axial compressor
|
| gptkbp:fan_art |
wide-chord fan
|
| gptkbp:first_flight |
gptkb:1985
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
annular combustor |
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Tay
|
| gptkbp:length |
3.5 m
|
| gptkbp:manufacturer |
gptkb:film_production_company
|
| gptkbp:number_of_stages |
5 stages
|
| gptkbp:propulsion |
18,500 lbf
|
| gptkbp:successor |
gptkb:Rolls-Royce_Trent_500
|
| gptkbp:type |
high-bypass turbofan
|
| gptkbp:used_in |
gptkb:Mc_Donnell_Douglas_MD-11
|
| gptkbp:weight |
3,000 kg
|