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gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:application
|
training aircraft
|
|
gptkbp:communityPartnerships
|
collaborations with aerospace companies
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:designedFor
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:drivetrain
|
training programs for operators
|
|
gptkbp:engine
|
air-cooled
low noise
innovative technology
air start
comprehensive support services
fuselage-mounted
regular updates and upgrades
|
|
gptkbp:engineConfiguration
|
global market presence
mass production
twin-spool
|
|
gptkbp:engineDisplacement
|
modular design
ongoing development
detailed technical documentation
|
|
gptkbp:engineType
|
high reliability
axial
high efficiency
turbojet engine
long service life
multiple variants available
certified by military authorities
single-stage high-pressure turbine
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
|
|
gptkbp:hasArea
|
extensive testing
|
|
gptkbp:hasContent
|
0.8 lb/hp/hr
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 4300
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:maxSpeed
|
0.8 Mach
|
|
gptkbp:missions
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:numberOfStudents
|
5
|
|
gptkbp:operationalArea
|
military training
|
|
gptkbp:producedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:propulsion
|
3,800 lbf
15.2_lbf/lb
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:revenue
|
1974
|
|
gptkbp:services
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:usedBy
|
gptkb:United_Arab_Emirates_Air_Force
gptkb:Kuwait_Air_Force
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Navy
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
gptkb:Oman_Air_Force
|
|
gptkbp:weight
|
250 kg
|