Properties (61)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turboshaft engine
|
| gptkbp:application |
helicopters
|
| gptkbp:certifications |
EASA_certified
|
| gptkbp:climate |
up to 1,000 °C
|
| gptkbp:compressionRatio |
16:1
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:design_feature |
modular design
|
| gptkbp:drivetrain |
reduction gearbox
|
| gptkbp:engine |
150 kg
1,200 mm 600 mm 400 mm single engine |
| gptkbp:engineConfiguration |
horizontal configuration
|
| gptkbp:engineType |
gptkb:Arriel_2B
2 turbocharged axial compressor single-stage turbine Arriel 2D Arriel 2M Arriel 2S Arriel 2C Arriel 2E Arriel 2F Arriel 2G Arriel 2H Arriel 2J Arriel 2K Arriel 2L Arriel 2N Arriel 2P Arriel 2Q Arriel 2R Arriel 2T Arriel 2U Arriel 2V Arriel 2W Arriel 2X Arriel 2Y Arriel 2Z |
| gptkbp:exhaustSystem |
free turbine
|
| gptkbp:fanEvents |
nickel-based superalloy
|
| gptkbp:firstFlight |
1980
|
| gptkbp:fuel_capacity |
200 kg/h
|
| gptkbp:fuelType |
gptkb:Jet_A-1
spark ignition electronic fuel control |
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Arriel 2
|
| gptkbp:launchSite |
electrical starter
|
| gptkbp:maintenance |
1,500 hours
|
| gptkbp:manufacturer |
gptkb:Safran_Helicopter_Engines
|
| gptkbp:notableUsers |
gptkb:Eurocopter_AS350
gptkb:Bell_407 AgustaWestland AW109 |
| gptkbp:operationalRange |
up to 20,000 ft
|
| gptkbp:performances |
3,000 hours
|
| gptkbp:powerOutput |
1,000 shp
|
| gptkbp:propulsion |
500 to 1,000 shp
6.67 shp/kg |
| gptkbp:weight |
approximately 150 kg
|