gptkbp:instanceOf
|
jet engine
|
gptkbp:aircraft
|
gptkb:BAE_Systems_Hawk
|
gptkbp:application
|
military training aircraft
|
gptkbp:coolingSystem
|
air-cooled
|
gptkbp:design_feature
|
modular design
|
gptkbp:developer
|
joint venture
|
gptkbp:diameter
|
approximately 0.9 m
|
gptkbp:emissionsStandard
|
low emissions
|
gptkbp:engineConfiguration
|
twin-spool
|
gptkbp:engineType
|
axial compressor
single-stage turbine
|
gptkbp:firstFlight
|
1974
|
gptkbp:firstRace
|
1970s
|
gptkbp:fuel_capacity
|
0.5 kg/lbf/hr
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 951-2
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
gptkbp:length
|
approximately 1.5 m
|
gptkbp:maintenance
|
1,000 hours
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
gptkbp:maximum_speed
|
Mach_0.9
|
gptkbp:noise_level
|
low noise
|
gptkbp:operational_status
|
gptkb:United_Arab_Emirates_Air_Force
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Navy
gptkb:Kuwaiti_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
gptkb:Oman_Air_Force
|
gptkbp:propulsion
|
13:1
approximately 4,000 lbf
|
gptkbp:related_engine
|
gptkb:Adour_Mk_951-20
gptkb:Adour_Mk_951-12
gptkb:Adour_Mk_951-19
gptkb:Adour_Mk_951-16
gptkb:Adour_Mk_951-18
gptkb:Adour_Mk_951
gptkb:Adour_Mk_951-6
gptkb:Adour_Mk_951-9
gptkb:Adour_Mk_951-7
gptkb:Adour_Mk_951-17
gptkb:Adour_Mk_951-11
gptkb:Adour_Mk_951-5
gptkb:Adour_Mk_951-13
gptkb:Adour_Mk_951-10
gptkb:Adour_Mk_951-8
gptkb:Adour_Mk_951-15
gptkb:Adour_Mk_951-14
gptkb:Adour_Mk_951-4
Brayton_cycle
|
gptkbp:service_ceiling
|
40,000 ft
|
gptkbp:successor
|
gptkb:Adour_Mk_951-3
|
gptkbp:type
|
turbofan engine
|
gptkbp:weight
|
approximately 300 kg
|