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gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:application
|
advanced jet trainer
military training aircraft
|
|
gptkbp:certifications
|
EASA_certified
|
|
gptkbp:climate
|
up to 900 °C
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engine
|
0.9 m
1.5 m
150 kg
military training aircraft
|
|
gptkbp:engineConfiguration
|
gptkb:Rolls-Royce
twin-shaft
twin-shaft turbofan
|
|
gptkbp:engineType
|
turbofan
axial
single_spool
|
|
gptkbp:fanBase
|
single stage fan
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuel_capacity
|
0.8 lb/hp/hr
100 lb/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
spark plug
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 32000
|
|
gptkbp:inspiration
|
gptkb:UK
|
|
gptkbp:introduced
|
1970s
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
75 dB
|
|
gptkbp:number_of_stages
|
8 stages
|
|
gptkbp:operationalRange
|
up to 30,000 ft
|
|
gptkbp:propulsion
|
21.3:1
3200 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_951
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:training
|
gptkb:Adour_engine_family
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
150 kg
|