Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
4.3:1 to 4.9:1
|
| gptkbp:certification |
1983
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
1.96 m
|
| gptkbp:family |
gptkb:RB211
|
| gptkbp:firstRun |
1980
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
RB211-535
|
| gptkbp:length |
3.89 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notableVariant |
gptkb:RB211-535C
gptkb:RB211-535E4 gptkb:RB211-535E4B gptkb:RB211-535E4C |
| gptkbp:numberOfStages |
14
3 |
| gptkbp:thrust |
37,400–43,100 lbf
|
| gptkbp:usedOn |
gptkb:Boeing_757
gptkb:Tupolev_Tu-204 |
| gptkbp:weight |
2,230 kg
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_RB211
|
| gptkbp:bfsLayer |
5
|