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gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
trainer aircraft
|
|
gptkbp:application
|
military training
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:designedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:developer
|
gptkb:Adour_Mk_951
gptkb:Adour_Mk_871
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engineType
|
axial
single_spool
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelCapacity
|
0.5 kg/kN/h
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 20000
|
|
gptkbp:launchSite
|
starter-generator
|
|
gptkbp:length
|
1.8 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:maxSpeed
|
Mach_0.9
|
|
gptkbp:noise_level
|
85 dB
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
|
|
gptkbp:produces
|
1970s
|
|
gptkbp:productionCompany
|
in production
|
|
gptkbp:propulsion
|
20 kN
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:relatedPatent
|
gptkb:Rolls-Royce_RB.168
gptkb:Rolls-Royce_RB.199
gptkb:Rolls-Royce_AE_3007
gptkb:Rolls-Royce_Spey
Rolls-Royce Trent
|
|
gptkbp:services
|
1976
|
|
gptkbp:setting
|
turbofan
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:totalGoals
|
over 2000
|
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
gptkb:BAE_Systems_Hawk
|
|
gptkbp:variant
|
gptkb:Adour_Mk_4000
gptkb:Adour_Mk_3000
gptkb:Adour_Mk_951
gptkb:Adour_Mk_2000
gptkb:Adour_Mk_871
|
|
gptkbp:weight
|
approximately 200 kg
|