|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
Hawk_family
|
|
gptkbp:application
|
trainer aircraft
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:designedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:engine
|
air-cooled
low noise
air start
rear fuselage
|
|
gptkbp:engineConfiguration
|
mass production
twin-spool
|
|
gptkbp:engineType
|
gptkb:Adour_Mk_151
gptkb:Adour_Mk_171-55
gptkb:Adour_Mk_171-50
gptkb:Adour_Mk_171-40
gptkb:Adour_Mk_171-25
gptkb:Adour_Mk_171-45
gptkb:Adour_Mk_171-65
gptkb:Adour_Mk_171-70
gptkb:Adour_Mk_171-30
gptkb:Adour_Mk_171-35
gptkb:Adour_Mk_171-60
modular design
high reliability
axial
single-stage
high thrust-to-weight ratio
|
|
gptkbp:fanBase
|
single-stage fan
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
|
|
gptkbp:hasArea
|
ground testing
|
|
gptkbp:hasContent
|
0.8 kg/kN/h
|
|
gptkbp:hasDepartment
|
no
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 171-28
|
|
gptkbp:length
|
1.8 m
|
|
gptkbp:maxSpeed
|
Mach_0.9
|
|
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:operationalRange
|
1,500 km
|
|
gptkbp:propulsion
|
28 kN
|
|
gptkbp:related_engine
|
brayton_cycle
|
|
gptkbp:services
|
1976
|
|
gptkbp:type
|
military engine
|
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:weight
|
150 kg
|