Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
8.5:1
|
| gptkbp:certification |
2001
|
| gptkbp:configuration |
three-shaft
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:family |
gptkb:Rolls-Royce_Trent
|
| gptkbp:firstRun |
1999
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Trent 500
|
| gptkbp:length |
4.37 m
|
| gptkbp:mainRotorDiameter |
2.47 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:numberOfStages |
IP: 1, HP: 1, LP: 5
IP: 8, HP: 6 |
| gptkbp:relatedTo |
gptkb:Trent_700
gptkb:Trent_800 gptkb:Trent_900 |
| gptkbp:status |
in service
|
| gptkbp:thrust |
53,000–60,000 lbf
|
| gptkbp:usedInAircraft |
gptkb:Airbus_A340-500
gptkb:aircraft |
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Holdings
|
| gptkbp:bfsLayer |
5
|