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gptkbp:instanceOf
|
turbojet engine
|
|
gptkbp:aircraft
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:communitySupport
|
modular engine design
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:developer
|
gptkb:Rolls-Royce_and_Turbomeca_collaboration
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
compliant_with_ICAO_standards
|
|
gptkbp:engineConfiguration
|
turbojet
|
|
gptkbp:engineType
|
axial
single_spool
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuel_capacity
|
high efficiency
0.85 lb/hp/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 2800
|
|
gptkbp:inspiration
|
gptkb:United_Kingdom
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:launchDate
|
30 seconds
|
|
gptkbp:length
|
3.4 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_feature
|
gptkb:Adour_Mk_871
|
|
gptkbp:operational_status
|
training and light attack missions
|
|
gptkbp:operationalHistory
|
used by several air forces
|
|
gptkbp:operationalRange
|
short-range
|
|
gptkbp:propulsion
|
7.0:1
2800 lbf
|
|
gptkbp:related_engine
|
Brayton_cycle
Adour_family
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:services
|
5000 hours
|
|
gptkbp:serviceType
|
1976
|
|
gptkbp:type
|
afterburning turbojet
|
|
gptkbp:weight
|
400 kg
|