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gptkbp:instanceOf
|
turbojet engine
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
axial
single-stage
Mk 171-100F
Mk 171-10F
Mk 171-110F
Mk 171-120F
Mk 171-140F
Mk 171-150F
Mk 171-170F
Mk 171-180F
Mk 171-190F
Mk 171-200F
Mk 171-20F
Mk 171-30F
Mk 171-40
Mk 171-40F
Mk 171-50F
Mk 171-70F
Mk 171-80F
Mk 171-90F
Mk_171-130F
Mk_171-160F
Mk_171-60F
|
|
gptkbp:exhaustSystem
|
subsonic
convergent-divergent
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuel_capacity
|
0.85 lb/hp/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 171-40F
|
|
gptkbp:inspiration
|
training and light attack
|
|
gptkbp:introduced
|
1974
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
3.2 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_status
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
|
|
gptkbp:propulsion
|
3,500 lbf
8.75
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_151
gptkb:Adour_Mk_171
Adour Mk 151-40F
Brayton_cycle
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:training
|
gptkb:British_Aerospace
|
|
gptkbp:type
|
afterburning turbojet
|
|
gptkbp:weight
|
400 kg
|