Turbomeca Arriel 1 S1

URI: https://gptkb.org/entity/Turbomeca_Arriel_1_S1
GPTKB entity
Statements (45)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application gptkb:Eurocopter_AS350
gptkb:Agusta_A109
gptkb:Eurocopter_EC120
gptkbp:certification gptkb:EASA
gptkb:FAA
gptkbp:combustor_type annular
gptkbp:compression_ratio 12:1
gptkbp:control_system gptkb:FADEC
gptkbp:cooling_system air-cooled
gptkbp:diameter 0.3 m
0.4 m
gptkbp:elevation up to 20,000 ft
gptkbp:engine_configuration free turbine
gptkbp:engine_power 500 shp
gptkbp:engine_type single-spool
turbo-shaft
gptkbp:exhaust_gas_temperature 650 ° C
gptkbp:first_flight gptkb:1980
gptkbp:fuel_capacity 120 kg
1.1 m
0.4 m
gptkbp:fuel_economy high
0.5 kg/s
gptkbp:fuel_type gptkb:Jet_A-1
gptkbp:gearbox reduction gearbox
https://www.w3.org/2000/01/rdf-schema#label Turbomeca Arriel 1 S1
gptkbp:ignition_system spark ignition
gptkbp:launch_window starter-generator
gptkbp:length 1.1 m
gptkbp:maintenance 500 hours
gptkbp:manufacturer gptkb:Turbomeca
gptkbp:noise_level low
gptkbp:operational_range -40 to 50 ° C
gptkbp:power_output 500 shp
gptkbp:predecessor gptkb:Arriel_1_B
gptkbp:propulsion 500 shp
2,000 N
gptkbp:service_entry gptkb:1980
gptkbp:successor gptkb:Arriel_2
gptkbp:turbine_type axial
gptkbp:type gptkb:turbofan_engine
gptkbp:used_in gptkb:Eurocopter_AS350
helicopters
gptkbp:weight 120 kg