|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:application
|
advanced jet trainer
military training aircraft
|
|
gptkbp:climate
|
up to 1,000 °C
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
low bypass ratio
|
|
gptkbp:developer
|
joint_venture_between_Rolls-Royce_and_Turbomeca
|
|
gptkbp:diameter
|
approximately 0.9 m
|
|
gptkbp:emissionsStandard
|
compliant_with_ICAO
|
|
gptkbp:engine
|
advanced technology
pylon-mounted
various military applications
|
|
gptkbp:engineConfiguration
|
turbojet engine
|
|
gptkbp:engineType
|
modular design
axial compressor
air start
single-stage turbine
multiple variants available
military turbofan engine
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuel_capacity
|
0.8 lb/lbf/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
hydromechanical system
|
|
gptkbp:hasDepartment
|
no
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 871-31L17
|
|
gptkbp:introduced
|
1970s
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
approximately 1.5 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
|
|
gptkbp:number_of_stages
|
8 stages
|
|
gptkbp:operationalRange
|
up to 30,000 ft
|
|
gptkbp:performances
|
high reliability
high efficiency
high thrust-to-weight ratio
detailed specifications available.
|
|
gptkbp:propulsion
|
2.92
approximately 3,500 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_871
|
|
gptkbp:services
|
up to 5,000 hours
|
|
gptkbp:setting
|
twin-spool
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:updates
|
upgraded versions available
|
|
gptkbp:weight
|
approximately 1,200 lb
|