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gptkbp:instanceOf
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jet engine
|
|
gptkbp:aircraft
|
Hawk_family
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:climate
|
1500 K
|
|
gptkbp:controls
|
electric starter
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
5000 hours
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
CAA
|
|
gptkbp:engine
|
twin-shaft
|
|
gptkbp:engineConfiguration
|
single_spool
|
|
gptkbp:engineType
|
axial
|
|
gptkbp:exhaustSystem
|
subsonic
convergent-divergent
|
|
gptkbp:firstRace
|
1964
|
|
gptkbp:fuel_capacity
|
can-type
0.8 kg/s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
spark ignition
dual fuel system
|
|
gptkbp:hasArea
|
flight testing
ground testing
|
|
gptkbp:historicalEvent
|
derived_from_Adour_Mk_100
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 500
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
3.1 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:modifications
|
upgraded to Mk 951
|
|
gptkbp:noise_level
|
low
|
|
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:number_of_stages
|
3
|
|
gptkbp:operational_status
|
1970s
|
|
gptkbp:operationalRole
|
trainer aircraft engine
|
|
gptkbp:performances
|
low maintenance costs
reliable operation
high thrust-to-weight ratio
good fuel efficiency
|
|
gptkbp:propulsion
|
33.3
5000 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_200
gptkb:Adour_Mk_951
gptkb:Adour_Mk_100
Brayton_cycle
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
150 kg
|