Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:Boeing_707
|
| gptkbp:compressor_type |
axial
|
| gptkbp:diameter |
68 in
3.0 ft |
| gptkbp:first_flight |
gptkb:1970
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
RB211-535
|
| gptkbp:length |
11.5 ft
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:number_of_stages |
gptkb:6
|
| gptkbp:operational_period |
two-spool
|
| gptkbp:propulsion |
22,000 lbf
|
| gptkbp:successor |
gptkb:RB211-535_E4
|
| gptkbp:turbine_type |
high-pressure turbine
|
| gptkbp:type |
high-bypass turbofan
|
| gptkbp:weight |
3,000 lb
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_RB211
|
| gptkbp:bfsLayer |
5
|