Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bypassRatio |
4.3:1
|
| gptkbp:certification |
1984
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
1.85 m
|
| gptkbp:family |
gptkb:Rolls-Royce_RB211
|
| gptkbp:firstRun |
1983
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:length |
3.89 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_plc
|
| gptkbp:notableFor |
improved fuel efficiency over earlier RB211 variants
|
| gptkbp:numberOfStages |
1 (HP), 1 (IP), 3 (LP)
3 (fan), 8 (IP), 6 (HP) |
| gptkbp:thrust |
40,100 lbf
|
| gptkbp:usedInAircraft |
gptkb:Boeing_757
gptkb:Tupolev_Tu-204 |
| gptkbp:weight |
2,260 kg
|
| gptkbp:bfsParent |
gptkb:Boeing_757-222
|
| gptkbp:bfsLayer |
5
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce RB211-535E4
|