|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
gptkb:Hawk_Mk_132
gptkb:Hawk_T1
Hawk 100
Hawk 200
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:collaborations
|
gptkb:British_Aerospace
|
|
gptkbp:controls
|
air start
digital control system
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
compliant_with_ICAO_standards
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
axial compressor
single-stage turbine
|
|
gptkbp:firstRace
|
1970
|
|
gptkbp:fuel_capacity
|
high fuel efficiency
0.8 kg/kN/h
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
hydromechanical fuel control
|
|
gptkbp:hasArea
|
extensively tested in various conditions
|
|
gptkbp:hasDepartment
|
no
|
|
gptkbp:historicalEvent
|
derived_from_Adour_Mk_811
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 822
|
|
gptkbp:inspiration
|
training and light attack
|
|
gptkbp:is_used_in
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:length
|
1.8 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:market_segment
|
military aviation
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low
|
|
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
|
short-range
up to 10,000 m
|
|
gptkbp:performances
|
approximately 3,000 hours
|
|
gptkbp:propulsion
|
0.11
22 kN
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_951
gptkb:Adour_Mk_871
gptkb:Adour_Mk_811
Brayton_cycle
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:serviceType
|
1976
|
|
gptkbp:successor
|
gptkb:Adour_Mk_871
|
|
gptkbp:team
|
Rolls-Royce_engineers
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 200 kg
|