Adour Mk 208

GPTKB entity

Statements (49)
Predicate Object
gptkbp:instanceOf jet engine
gptkbp:accessories temperature sensors
control unit
pressure sensors
fuel pump
oil pump
vibration sensors
thrust reverser
fuel flow meter
starter generator
gptkbp:aircraft gptkb:BAE_Systems_Hawk
gptkbp:application military training aircraft
gptkbp:controls digital electronic control
starter motor
gptkbp:coolingSystem air-cooled
gptkbp:diameter 0.9 m
gptkbp:emissionsStandard compliant_with_ICAO_standards
gptkbp:engineConfiguration twin-spool
gptkbp:engineType axial compressor
single-stage turbine
gptkbp:firstRace 1964
gptkbp:fuel_capacity 0.85 kg/kN/h
gptkbp:fuelType gptkb:Jet_A-1
spark ignition
annular combustor
hydromechanical fuel control
https://www.w3.org/2000/01/rdf-schema#label Adour Mk 208
gptkbp:is_used_in gptkb:Hawker_Siddeley_Hawk
gptkbp:length 1.5 m
gptkbp:maintenance 200 hours
gptkbp:manufacturer gptkb:Rolls-Royce
gptkbp:maximum_speed Mach_0.9
gptkbp:noise_level low noise
gptkbp:operational_status gptkb:United_Arab_Emirates_Air_Force
gptkb:Indian_Air_Force
gptkb:Qatar_Emiri_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Navy
gptkb:Kuwaiti_Air_Force
gptkb:Omani_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
gptkbp:propulsion 20 kN
gptkbp:related_engine Brayton_cycle
gptkbp:services approximately 3,000 hours
gptkbp:successor gptkb:Adour_Mk_871
gptkbp:type turbofan engine
gptkbp:weight approximately 200 kg