|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
Hawk_family
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:constructionMaterial
|
lightweight alloys
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
air cooling
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
Euro I
|
|
gptkbp:engine
|
modular components
rear-mounted
|
|
gptkbp:engineConfiguration
|
twin-spool
completed successfully.
|
|
gptkbp:engineType
|
high
axial
single stage
|
|
gptkbp:environmental_impact
|
low emissions
|
|
gptkbp:exhaustSystem
|
variable geometry
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:firstRace
|
1970
|
|
gptkbp:fuel_capacity
|
high
1,200 lb/hr
0.8 lb/hp/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
dual fuel pumps
|
|
gptkbp:hasArea
|
conducted_at_Rolls-Royce_facilities
|
|
gptkbp:historicalEvent
|
derived_from_the_Rolls-Royce_Spey
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 4200
|
|
gptkbp:internationalRelations
|
gptkb:United_Kingdom
|
|
gptkbp:is_a_source_of
|
trainer aircraft
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
3.1 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:market_segment
|
military training
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low
achieved through design
|
|
gptkbp:notable_feature
|
gptkb:Adour_Mk_871
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_status
|
gptkb:Royal_Air_Force
|
|
gptkbp:operationalRange
|
1,000 km
|
|
gptkbp:performances
|
3,000 hours
scheduled every 1,500 hours
|
|
gptkbp:propulsion
|
28:1
4200 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_951
Brayton_cycle
|
|
gptkbp:reviews
|
excellent
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
150 kg
|