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gptkbp:instanceOf
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jet engine
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|
gptkbp:aircraft
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gptkb:BAE_Systems_Hawk
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:controls
|
digital electronic control
starter-generator
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design_feature
|
modular construction
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|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
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gptkbp:engine
|
rear-mounted
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
axial
afterburning turbofan
|
|
gptkbp:exhaustSystem
|
variable geometry
|
|
gptkbp:fuel_capacity
|
0.8 kg/s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
dual fuel system
|
|
gptkbp:historicalEvent
|
derived_from_Adour_Mk_100
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 17000
|
|
gptkbp:inspiration
|
training and light attack
|
|
gptkbp:introduced
|
1970s
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
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:Royal_Navy
gptkb:South_African_Air_Force
|
|
gptkbp:number_of_stages
|
3
|
|
gptkbp:operational_status
|
in service
training and light attack missions
|
|
gptkbp:operationalRange
|
1,000 km
|
|
gptkbp:origin
|
gptkb:United_Kingdom
|
|
gptkbp:performances
|
3000 hours
|
|
gptkbp:propulsion
|
17000 lbf
43:1
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_151
gptkb:Adour_Mk_200
gptkb:Adour_Mk_300
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 400 kg
|