|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
trainer aircraft
|
|
gptkbp:application
|
advanced jet trainer
|
|
gptkbp:climate
|
high temperature
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
modular design
|
|
gptkbp:developer
|
gptkb:Adour_engine_family
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
low emissions
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
axial compressor
single-stage turbine
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuel_capacity
|
high fuel efficiency
0.8 lb/hp/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 171-40B
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_feature
|
advanced materials
high thrust-to-weight ratio
digital control system
modular maintenance
versatile application
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
|
|
gptkbp:operational_status
|
in production
|
|
gptkbp:operationalHistory
|
used by several air forces
|
|
gptkbp:produces
|
over 1,000 units
|
|
gptkbp:productionLocation
|
1974
|
|
gptkbp:productionYears
|
1970s
|
|
gptkbp:propulsion
|
3,500 lbf
11.67
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_171-40D
gptkb:Adour_Mk_151
gptkb:Adour_Mk_171-40E
gptkb:Adour_Mk_171-40A
Brayton_cycle
Adour_family
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:serviceType
|
still in service
|
|
gptkbp:successor
|
gptkb:Adour_Mk_171-40C
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
300 kg
|