Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Boeing_777-200
|
| gptkbp:bypassRatio |
6.4:1
|
| gptkbp:certification |
1996
|
| gptkbp:compressor_stages |
IP: 8, HP: 6
|
| gptkbp:configuration |
three-shaft
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:family |
gptkb:Rolls-Royce_Trent
|
| gptkbp:firstRun |
1995
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Trent 892
|
| gptkbp:length |
4.37 m
|
| gptkbp:mainRotorDiameter |
2.79 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_plc
|
| gptkbp:relatedModel |
gptkb:Rolls-Royce_Trent_884
gptkb:Rolls-Royce_Trent_895 |
| gptkbp:thrust |
89,000 lbf
|
| gptkbp:turbine_stages |
HP: 1, IP: 1, LP: 6
|
| gptkbp:used_in |
gptkb:Boeing_777-200
|
| gptkbp:weight |
6,120 kg
|
| gptkbp:bfsParent |
gptkb:MH17
gptkb:MH370 |
| gptkbp:bfsLayer |
6
|