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gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:climate
|
1,000 °C
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design_feature
|
modular construction
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
gptkb:Adour_Mk_1200
gptkb:Adour_Mk_951
gptkb:Adour_Mk_1500
gptkb:Adour_Mk_1000
gptkb:Adour_Mk_871
axial
air start
single stage
|
|
gptkbp:fuel_capacity
|
1,200 lb/hr
0.8 lb/hp/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
dual fuel system
|
|
gptkbp:historicalEvent
|
derived_from_the_Rolls-Royce_Spey
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 4400
|
|
gptkbp:introduced
|
1970s
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
85 dB
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Saudi_Air_Force
gptkb:South_African_Air_Force
|
|
gptkbp:number_of_stages
|
8
|
|
gptkbp:operational_status
|
training and light attack missions
|
|
gptkbp:performances
|
3,000 hours
every 1,500 hours
|
|
gptkbp:propulsion
|
3.33
4,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
1,200 lb
|