|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
Hawk_family
|
|
gptkbp:application
|
military training
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
compliant_with_ICAO_standards
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
axial compressor
single-stage turbine
|
|
gptkbp:fuel_capacity
|
0.8 kg/s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustion chamber
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 871-31K-8B
|
|
gptkbp:introduced
|
1970s
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1.8 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operational_status
|
gptkb:Royal_Air_Force
|
|
gptkbp:operationalRange
|
1,500 km
|
|
gptkbp:propulsion
|
8.75:1
approximately 3,500 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_871
Brayton_cycle
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 400 kg
|