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gptkbp:instanceOf
|
turbo-shaft engine
|
|
gptkbp:application
|
helicopters
|
|
gptkbp:availability
|
widely available
|
|
gptkbp:certifications
|
EASA_certified
|
|
gptkbp:climate
|
-40 to 50 °C
|
|
gptkbp:compressionRatio
|
12:1
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
compact design
|
|
gptkbp:developer
|
developed_in_France
|
|
gptkbp:diameter
|
0.4 m
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engine
|
low
|
|
gptkbp:engineConfiguration
|
single-shaft
|
|
gptkbp:engineType
|
free turbine
1,000 °C
|
|
gptkbp:firstFlight
|
1970
|
|
gptkbp:fuel_capacity
|
high fuel efficiency
200 kg/h
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
dual ignition
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbomeca TM 319
|
|
gptkbp:is_used_in
|
gptkb:Eurocopter_AS350
|
|
gptkbp:launchSite
|
electric starter
|
|
gptkbp:legal_principle
|
gas turbine principle
|
|
gptkbp:length
|
1.2 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Turbomeca
|
|
gptkbp:market
|
civil aviation
readily available
|
|
gptkbp:noise_level
|
85 dB
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_status
|
military and civilian use
|
|
gptkbp:performances
|
3,000 hours
|
|
gptkbp:powerOutput
|
700 shp
|
|
gptkbp:propulsion
|
700 lbf
|
|
gptkbp:related_engine
|
gptkb:TM_family_of_engines
Brayton_cycle
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
20,000 ft
|
|
gptkbp:status
|
in production
|
|
gptkbp:successor
|
gptkb:Turbomeca_Arriel
|
|
gptkbp:supports
|
global support network
|
|
gptkbp:training
|
pilot training available
|
|
gptkbp:type
|
turbo-shaft engine
|
|
gptkbp:weight
|
150 kg
|