Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:bypass_ratio |
8:1
|
| gptkbp:controls |
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
2.9 m
2.7 m |
| gptkbp:emissions_standard |
CAEP/6
|
| gptkbp:engine_type |
gptkb:6
2 turbofan |
| gptkbp:first_flight |
gptkb:1995
|
| gptkbp:fuel_capacity |
0.5 lb/hp/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Trent 800 F
|
| gptkbp:length |
3.4 m
|
| gptkbp:maintenance |
4,000 hours
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:max_speed |
Mach 0.84
|
| gptkbp:noise_level |
Stage 3 compliant
|
| gptkbp:operational_range |
5,000 nautical miles
|
| gptkbp:propulsion |
80,000 lbf
|
| gptkbp:service_ceiling |
43,000 ft
|
| gptkbp:successor |
Trent 900
|
| gptkbp:used_in |
gptkb:aircraft
|
| gptkbp:weight |
4,000 kg
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Trent_800
|
| gptkbp:bfsLayer |
4
|