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gptkbp:instanceOf
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jet engine
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gptkbp:accessories
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integrated accessories gearbox
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gptkbp:aircraft
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gptkb:Hawker_Siddeley_Hawk_200
gptkb:BAE_Systems_Hawk
gptkb:Hawker_Siddeley_Hawk_T.1
Hawker Siddeley Hawk 100
Hawk_family
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|
gptkbp:application
|
military training aircraft
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gptkbp:certifications
|
civil and military certification
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gptkbp:collaborations
|
gptkb:British_Aerospace
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gptkbp:controls
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gptkb:full_authority_digital_engine_control_(FADEC)
air start
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gptkbp:coolingSystem
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air-cooled
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gptkbp:design_feature
|
modular design
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gptkbp:developer
|
Rolls-Royce Adour
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gptkbp:diameter
|
approximately 0.9 m
|
|
gptkbp:emissionsStandard
|
low emissions
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gptkbp:engineConfiguration
|
twin-spool
|
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gptkbp:engineType
|
axial compressor
single-stage turbine
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gptkbp:firstFlight
|
1974
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gptkbp:firstRace
|
1970s
|
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gptkbp:fuel_capacity
|
0.8 lb/hp/hr
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gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
dual ignition system
dual fuel system
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 871-31L2
|
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gptkbp:is_used_in
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gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
approximately 1.5 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:market
|
defense market
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operational_status
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Navy
gptkb:South_African_Air_Force
|
|
gptkbp:operationalRange
|
long operating range
|
|
gptkbp:produces
|
in production
over 1,000 units
|
|
gptkbp:propulsion
|
approximately 3,500 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_951
gptkb:Adour_Mk_871
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:supports
|
global support network
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 400 lb
|