Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:Boeing_707
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
2.5 m
|
| gptkbp:first_flight |
gptkb:1983
|
| gptkbp:fuel_economy |
0.5 lb/hp/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
RB211-535 E4
|
| gptkbp:length |
3.5 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:number_of_stages |
gptkb:6
|
| gptkbp:propulsion |
53,000 lbf
|
| gptkbp:turbine_type |
high bypass ratio
|
| gptkbp:weight |
3,000 kg
|
| gptkbp:bfsParent |
gptkb:Boeing_757-200_F
gptkb:RB211_engine gptkb:RB211-535 |
| gptkbp:bfsLayer |
6
|