Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:Flight
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
1.2 m
|
| gptkbp:engine_configuration |
twin-engine
|
| gptkbp:fan_art |
single-spool fan
|
| gptkbp:first_flight |
gptkb:1964
|
| gptkbp:fuel_economy |
0.8 kg/k N·h
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Spey 800
|
| gptkbp:length |
4.5 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:max_speed |
Mach 0.85
|
| gptkbp:operational_use |
commercial aviation
|
| gptkbp:propulsion |
80 k N
|
| gptkbp:successor |
gptkb:Rolls-Royce_RB.183
|
| gptkbp:turbine_type |
single-stage turbine
|
| gptkbp:type |
civil aircraft engine
|
| gptkbp:used_in |
gptkb:Mc_Donnell_Douglas_DC-10
|
| gptkbp:weight |
1,200 kg
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Spey_202
|
| gptkbp:bfsLayer |
5
|