Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Avon
|
| gptkbp:application |
regional aircraft
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:design |
gptkb:Embraer_ERJ_series
gptkb:Bombardier_CRJ_series |
| gptkbp:diameter |
1,000 mm
1,500 mm |
| gptkbp:engine_type |
axial compressor
high-pressure turbine |
| gptkbp:first_flight |
gptkb:1995
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
annular combustor |
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce RB.145
|
| gptkbp:length |
1,800 mm
|
| gptkbp:manufacturer |
gptkb:film_production_company
|
| gptkbp:propulsion |
20,000 lbf
|
| gptkbp:successor |
gptkb:Rolls-Royce_AE_3007
|
| gptkbp:type |
dual-spool engine
|
| gptkbp:weight |
1,200 lb
|