Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Trent_800
|
| gptkbp:bypass_ratio |
5.5:1
|
| gptkbp:certification |
CAEP/6
|
| gptkbp:controls |
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
| gptkbp:diameter |
2.7 m
2.68 m |
| gptkbp:engine_type |
gptkb:6
2 turbofan |
| gptkbp:first_flight |
gptkb:1994
|
| gptkbp:fuel_capacity |
0.5 lb/lbf/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Trent 800 I
|
| gptkbp:length |
3.5 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:noise_level |
Chapter 4
|
| gptkbp:propulsion |
100,000 lbf
80,000 lbf |
| gptkbp:services |
gptkb:1995
|
| gptkbp:setting |
high bypass ratio
|
| gptkbp:used_in |
gptkb:aircraft
|
| gptkbp:weight |
4,000 kg
|