|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:designedFor
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:developer
|
joint_venture_between_Rolls-Royce_and_Turbomeca
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
low emissions
|
|
gptkbp:engine
|
air start
pylon-mounted
|
|
gptkbp:engineConfiguration
|
twin-spool
single engine
twin engine
|
|
gptkbp:engineType
|
turbofan engine
turbojet engine
axial compressor
turboprop engine
axial turbine
helicopter engine
military engine
business jet engine
civil engine
commercial engine
general aviation engine
regional jet engine
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
dual fuel system
|
|
gptkbp:hasArea
|
flight testing
ground testing
|
|
gptkbp:hasContent
|
0.85 lb/hp/hr
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 16000
|
|
gptkbp:length
|
3.1 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:noise_level
|
low noise
|
|
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:numberOfStudents
|
8
|
|
gptkbp:numberOfTeams
|
2
|
|
gptkbp:operationalArea
|
training and light attack missions
|
|
gptkbp:producedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:propulsion
|
no thrust vectoring
16000 lbf
|
|
gptkbp:services
|
5000 hours
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:variant
|
gptkb:Adour_Mk_951
gptkb:Adour_Mk_1000
gptkb:Adour_Mk_871
|
|
gptkbp:weight
|
400 kg
|