Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
8.5:1
|
| gptkbp:certification |
October 2004
|
| gptkbp:configuration |
three-shaft
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
2.95 m
|
| gptkbp:family |
gptkb:Rolls-Royce_Trent
|
| gptkbp:firstFlight |
April 2005
|
| gptkbp:firstRun |
2003
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Trent 900
|
| gptkbp:length |
4.99 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notableEvent |
gptkb:Qantas_Flight_32_engine_failure
|
| gptkbp:numberOfStages |
IP: 1, HP: 1, LP: 6
IP: 8, HP: 6 |
| gptkbp:successor |
gptkb:Trent_XWB
|
| gptkbp:thrust |
311–356 kN
|
| gptkbp:usedIn |
gptkb:aircraft
|
| gptkbp:weight |
6,120 kg
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Holdings
|
| gptkbp:bfsLayer |
5
|