Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypass_ratio |
5.5:1
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
3.0 ft
66 in |
| gptkbp:engine_type |
axial compressor
two-stage turbine |
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Tay 611-8
|
| gptkbp:length |
12.5 ft
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:original_run |
gptkb:1980
|
| gptkbp:propulsion |
6110 lbf
|
| gptkbp:type |
high-bypass turbofan
|
| gptkbp:weight |
1500 lb
|
| gptkbp:bfsParent |
gptkb:Gulfstream_GIV-SP
gptkb:Gulfstream_G400 gptkb:Gulfstream_GIV gptkb:Gulfstream_V gptkb:Gulfstream_IV |
| gptkbp:bfsLayer |
4
|