Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:Boeing_757
gptkb:Tupolev_Tu-204 |
| gptkbp:bypassRatio |
4.3–4.94:1
|
| gptkbp:certification |
1983
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
1.85 m
|
| gptkbp:family |
gptkb:Rolls-Royce_RB211
|
| gptkbp:firstRun |
1977
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:length |
3.89 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_plc
|
| gptkbp:market |
commercial aviation
|
| gptkbp:notableVariant |
gptkb:RB211-535C
gptkb:RB211-535E4 gptkb:RB211-535E4B gptkb:RB211-535E4C |
| gptkbp:numberOfStages |
1-stage HP, 1-stage IP, 3-stage LP
3-stage fan, 1-stage LP, 7-stage IP, 6-stage HP |
| gptkbp:predecessor |
Rolls-Royce RB211-22B
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:Rolls-Royce_Trent_700
|
| gptkbp:thrust |
37,400–43,100 lbf
|
| gptkbp:usedOn |
gptkb:Boeing_757-200
gptkb:Boeing_757-300 Tupolev Tu-204-120 |
| gptkbp:weight |
2,260 kg
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_jet_engines
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce RB211-535
|