Properties (50)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbojet engine
|
| gptkbp:application |
helicopters
|
| gptkbp:climate |
-40 to 50 °C
|
| gptkbp:compressionRatio |
6:1
|
| gptkbp:controls |
mechanical control system
|
| gptkbp:coolingSystem |
air
air-cooled |
| gptkbp:design |
French_design
|
| gptkbp:developer |
developed in the 1950s
|
| gptkbp:diameter |
0.4 m
|
| gptkbp:drivetrain |
reduction gearbox
|
| gptkbp:emissionsStandard |
ICAO_Chapter_4
|
| gptkbp:engine |
horizontal layout
single engine Artouste IIIB model used in light helicopters |
| gptkbp:engineConfiguration |
free turbine configuration
single_spool |
| gptkbp:engineType |
turbo-shaft engine
free turbine starter motor 1,000 °C Artouste IIIB variant |
| gptkbp:exhaustSystem |
600 °C
|
| gptkbp:firstFlight |
1960
|
| gptkbp:fuel_capacity |
high fuel efficiency
0.5 kg/s |
| gptkbp:fuelType |
gptkb:Jet_A-1
spark ignition annular combustor dual fuel system |
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Artouste IIIB
|
| gptkbp:is_used_in |
gptkb:Aérospatiale_SA_315_Lama
|
| gptkbp:length |
1.2 m
|
| gptkbp:maintenance |
500 hours
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:market |
aerospace industry
|
| gptkbp:noise_level |
85 dB
|
| gptkbp:operationalHistory |
used in military and civilian aircraft
|
| gptkbp:performances |
1,500 hours
high performance engine |
| gptkbp:powerOutput |
370 kW
|
| gptkbp:propulsion |
500 shp
3.1 kW/kg |
| gptkbp:related_engine |
Artouste_family
|
| gptkbp:reliability |
high reliability
|
| gptkbp:service_ceiling |
3,000 m
|
| gptkbp:successor |
gptkb:Turbomeca_Arriel
|
| gptkbp:type |
turbo-shaft engine
|
| gptkbp:weight |
120 kg
|