|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:airlines
|
25 kg/s
|
|
gptkbp:application
|
trainer aircraft
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:design
|
modular design
|
|
gptkbp:designedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:developer
|
joint venture
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
low emissions
|
|
gptkbp:engine
|
rear-mounted
air start
|
|
gptkbp:engineConfiguration
|
twin-shaft
|
|
gptkbp:engineType
|
turbojet
axial
single_spool
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustion chamber
hydromechanical fuel control
|
|
gptkbp:hasContent
|
0.8 kg/kN·h
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 1100
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:market
|
military aviation
|
|
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:operationalArea
|
military training
|
|
gptkbp:performance
|
high reliability
|
|
gptkbp:powerOutput
|
820 kW
|
|
gptkbp:propulsion
|
no thrust vectoring
1100 lbf
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:relatedPatent
|
gptkb:Adour_Mk_151
gptkb:Adour_Mk_100
gptkb:Adour_Mk_202
|
|
gptkbp:retirementYear
|
still in service
|
|
gptkbp:services
|
1976
|
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
|
gptkbp:type
|
military engine
|
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:weight
|
200 kg
|