Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
regional aircraft
|
| gptkbp:armament |
gptkb:6
|
| gptkbp:compression_ratio |
16:1
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:design_uses |
twin-engine aircraft
|
| gptkbp:diameter |
1,200 mm
|
| gptkbp:engine_configuration |
free turbine
|
| gptkbp:engine_type |
turboprop
|
| gptkbp:first_flight |
gptkb:1994
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce AE 2100
|
| gptkbp:length |
1,800 mm
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:max_speed |
400 knots
|
| gptkbp:notable_users |
gptkb:Bombardier
gptkb:Lockheed_Martin gptkb:Embraer |
| gptkbp:operational_range |
1,500 nautical miles
|
| gptkbp:power_output |
up to 4,600 shp
|
| gptkbp:propulsion |
3.83
|
| gptkbp:type_of |
gptkb:turbofan_engine
|
| gptkbp:weight |
approximately 1,200 lb
|
| gptkbp:bfsParent |
gptkb:Airbus_A400_M
|
| gptkbp:bfsLayer |
5
|