|
gptkbp:instanceOf
|
turbojet engine
|
|
gptkbp:application
|
civil aviation
|
|
gptkbp:compressionRatio
|
20:1
|
|
gptkbp:constructionMaterial
|
subsonic intake
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:documentType
|
variable area nozzle
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engine
|
150 kg
85 dB
military aircraft
high reliability
pylon-mounted
|
|
gptkbp:engineConfiguration
|
axial-flow
single_spool
|
|
gptkbp:engineType
|
turbojet engine
single-stage turbine
excellent performance
TM319-1
EASA_certified
|
|
gptkbp:firstFlight
|
1970
|
|
gptkbp:fuelCapacity
|
0.5 kg/kW·h
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
spark ignition
dual fuel system
|
|
gptkbp:generator
|
1200 °C
|
|
gptkbp:hasArea
|
Turbomeca_test_facility
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbomeca TM319
|
|
gptkbp:launchSite
|
electric starter
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Turbomeca
|
|
gptkbp:maximumDepth
|
900 °C
|
|
gptkbp:maxSpeed
|
12000 rpm
|
|
gptkbp:numberOfStudents
|
3
|
|
gptkbp:operationalRange
|
high_altitude
|
|
gptkbp:operationalStatus
|
tropical
30 psi
|
|
gptkbp:performances
|
3000 hours
|
|
gptkbp:powerOutput
|
2400 kW
|
|
gptkbp:propulsion
|
16:1
3190 lbf
|
|
gptkbp:services
|
6000 m
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:usedIn
|
gptkb:Eurocopter_AS350
|
|
gptkbp:weight
|
150 kg
|