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gptkbp:instanceOf
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jet engine
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gptkbp:aircraft
|
gptkb:BAE_Systems_Hawk
|
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gptkbp:application
|
military training aircraft
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|
gptkbp:certifications
|
certified by various aviation authorities
|
|
gptkbp:climate
|
up to 1,500 °C
|
|
gptkbp:constructionMaterial
|
advanced composite materials
|
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gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engine
|
rear-mounted engine
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
axial compressor
air start
single-stage turbine
|
|
gptkbp:environmental_impact
|
low environmental impact
|
|
gptkbp:exhaustSystem
|
convergent exhaust
fixed air intake
|
|
gptkbp:fuel_capacity
|
high fuel efficiency
0.8 kg/kN/h
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
dual fuel system
|
|
gptkbp:future_plans
|
potential upgrades planned.
|
|
gptkbp:hasArea
|
extensively tested
|
|
gptkbp:historicalEvent
|
derived_from_Adour_Mk_151
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 171-50
|
|
gptkbp:introduced
|
1970s
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1.8 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:market_segment
|
military aviation market
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Navy
gptkb:South_African_Air_Force
|
|
gptkbp:operational_status
|
training and light attack missions
|
|
gptkbp:operationalRange
|
up to 90% of maximum thrust
|
|
gptkbp:propulsion
|
high power-to-weight ratio
50 kN
no thrust vectoring
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:services
|
up to 5,000 hours
|
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
|
gptkbp:team
|
Rolls-Royce_design_team
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 200 kg
|