Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:application |
helicopters
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:design |
twin-spool design
|
| gptkbp:engine_type |
axial compressor
single-stage turbine |
| gptkbp:first_flight |
gptkb:1997
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Arriel 2 E
|
| gptkbp:maintenance |
1,500 hours
|
| gptkbp:manufacturer |
gptkb:Safran_Helicopter_Engines
|
| gptkbp:notable_users |
Eurocopter E C135
Agusta Westland A W109 |
| gptkbp:operational_range |
varies by aircraft
|
| gptkbp:power_output |
up to 1,000 shp
|
| gptkbp:propulsion |
500 to 1,100 lbf
|
| gptkbp:weight |
approximately 150 kg
|
| gptkbp:bfsParent |
gptkb:Arriel_engine
|
| gptkbp:bfsLayer |
6
|