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gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
Hawk_family
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:climate
|
1,500 °F
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:diameter
|
approximately 0.9 m
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
axial compressor
single-stage turbine
|
|
gptkbp:facilities
|
gptkb:Rolls-Royce_test_facilities
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:firstRace
|
1970s
|
|
gptkbp:fuel_capacity
|
0.8 lb/hp/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
spark ignition
|
|
gptkbp:future_plans
|
limited production
|
|
gptkbp:historicalEvent
|
developed_from_Adour_Mk_151
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 171-47
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
approximately 1.5 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
subsonic
|
|
gptkbp:militaryRank
|
gptkb:Royal_Navy
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_feature
|
gptkb:Adour_Mk_151
|
|
gptkbp:operational_status
|
gptkb:Royal_Air_Force
|
|
gptkbp:operator
|
none
|
|
gptkbp:origin
|
gptkb:United_Kingdom
|
|
gptkbp:propulsion
|
8.75:1
approximately 3,500 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_171
Brayton_cycle
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
30,000 ft
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
|
gptkbp:training
|
ground support equipment
Adour engine program
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 400 lb
|