|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:certifications
|
EASA_certified
|
|
gptkbp:climate
|
up to 1,500 °C
|
|
gptkbp:constructionMaterial
|
composite materials
titanium
steel alloys
aluminum alloys
nickel alloys
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engine
|
twin-spool
|
|
gptkbp:engineConfiguration
|
turbojet
|
|
gptkbp:engineType
|
axial
jet engine
|
|
gptkbp:environmental_impact
|
low emissions
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuel_capacity
|
high
0.85 lb/lbf/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
gptkbp:future_plans
|
upgraded variants
|
|
gptkbp:hasArea
|
gptkb:Rolls-Royce_test_facility
|
|
gptkbp:historicalEvent
|
derived_from_Adour_Mk_100
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 3300Z
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:market_segment
|
military aviation
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notableUsers
|
gptkb:Kuwait_Air_Force
gptkb:Indian_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
|
|
gptkbp:number_of_stages
|
5
|
|
gptkbp:operational_status
|
gptkb:Royal_Air_Force
in production
|
|
gptkbp:propulsion
|
22:1
3300 lbf
|
|
gptkbp:related_engine
|
Adour_family
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:team
|
Rolls-Royce_engineers
|
|
gptkbp:training
|
joint venture
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:weight
|
150 kg
|