Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
6.4:1
|
| gptkbp:certification |
1996
|
| gptkbp:compressionRatio |
39:1
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:family |
gptkb:Rolls-Royce_Trent
|
| gptkbp:firstRun |
1993
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:length |
4.37 m
|
| gptkbp:mainRotorDiameter |
2.8 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notableEvent |
gptkb:British_Airways_Flight_38
|
| gptkbp:numberOfAxles |
3
|
| gptkbp:numberOfStages |
6 (HP, IP, LP)
8 (HP) |
| gptkbp:predecessor |
gptkb:Trent_700
|
| gptkbp:successor |
gptkb:Trent_1000
|
| gptkbp:thrust |
75,000 to 95,000 lbf
|
| gptkbp:usedOn |
gptkb:Boeing_777
|
| gptkbp:weight |
7,400 kg
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Holdings
|
| gptkbp:bfsLayer |
5
|
| https://www.w3.org/2000/01/rdf-schema#label |
Trent 800
|