Statements (15)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:Turbomeca_Arriel_2_D
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:compression_ratio |
16:1
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:engine |
twin-spool
|
| gptkbp:first_flight |
gptkb:1980s
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Arriel 2 S
|
| gptkbp:manufacturer |
gptkb:Safran_Helicopter_Engines
|
| gptkbp:power_output |
500 shp
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
Eurocopter A S350
|
| gptkbp:weight |
120 kg
|