|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
helicopters
|
|
gptkbp:average_temperature
|
up to 800 ° C
|
|
gptkbp:certification
|
EASA certified
|
|
gptkbp:compression_ratio
|
6:1
|
|
gptkbp:control_system
|
hydromechanical control
|
|
gptkbp:cooling_system
|
air-cooled
direct air cooling
|
|
gptkbp:design
|
modular design
|
|
gptkbp:diameter
|
0.4 m
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
light helicopter engine
|
|
gptkbp:engine_configuration
|
free turbine
|
|
gptkbp:engine_power
|
1500 hours
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
|
|
gptkbp:exhaust_system
|
axial exhaust
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_economy
|
high
0.5 kg/k Wh
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox_ratio
|
3.5:1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbomeca Artouste IIIB
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:length
|
1.2 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Turbomeca
|
|
gptkbp:market_segment
|
gptkb:civil_aviation
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:operational_range
|
500 km
|
|
gptkbp:power_output
|
370 k W
|
|
gptkbp:propulsion
|
500 shp
|
|
gptkbp:reliability
|
high
|
|
gptkbp:rotor_speed
|
4000 rpm
|
|
gptkbp:service_history
|
widely used in military and civilian applications.
|
|
gptkbp:starting_system
|
electric starter
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Aérospatiale_Alouette_III
|
|
gptkbp:vibration_level
|
low
|
|
gptkbp:weight
|
120 kg
|
|
gptkbp:year_established
|
gptkb:1960
|
|
gptkbp:bfsParent
|
gptkb:Chetak_helicopters
gptkb:SA_316_Alouette_III
|
|
gptkbp:bfsLayer
|
7
|