|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:climate
|
1,500 °F
|
|
gptkbp:controls
|
starter-generator
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
3,000 hours
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:emissionsStandard
|
compliant_with_ICAO
|
|
gptkbp:engine
|
modular design
rear-mounted
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
axial compressor
single-stage turbine
Adour_Mk_171-40G-1
Adour_Mk_171-40G-10
Adour_Mk_171-40G-2
Adour_Mk_171-40G-3
Adour_Mk_171-40G-4
Adour_Mk_171-40G-5
Adour_Mk_171-40G-6
Adour_Mk_171-40G-7
Adour_Mk_171-40G-8
Adour_Mk_171-40G-9
|
|
gptkbp:exhaustSystem
|
mixed-flow intake
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuel_capacity
|
0.85 lb/hp/hr
1,000 lb/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
hydromechanical
|
|
gptkbp:hasArea
|
static test
flight test
|
|
gptkbp:hasDepartment
|
no
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 171-40G
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low noise
|
|
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
|
14:1
3,500 lbf
14.0 lbf/kg
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
250 kg
|