|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
gptkb:Hawk_T1
trainer aircraft
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:design
|
modular design
to power advanced jet trainers.
|
|
gptkbp:designedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:developer
|
joint_development_with_British_Aerospace
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
low emissions
|
|
gptkbp:energyEfficiency
|
high fuel efficiency
|
|
gptkbp:engine
|
pylon-mounted
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
turbojet engine
axial compressor
single-stage turbine
|
|
gptkbp:exportedTo
|
several countries
|
|
gptkbp:firstFlight
|
1980s
|
|
gptkbp:fuelCapacity
|
low fuel consumption
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 214
|
|
gptkbp:keyIssues
|
high thrust-to-weight ratio
|
|
gptkbp:launchSite
|
air start
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:market
|
military aviation market
|
|
gptkbp:maxSpeed
|
Mach_0.9
|
|
gptkbp:modifications
|
various upgrades available
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:numberOfStudents
|
two
|
|
gptkbp:operationalArea
|
training and light attack missions
|
|
gptkbp:operationalStatus
|
in service
up to 40,000 ft
|
|
gptkbp:productionCompany
|
1970s to 1980s
|
|
gptkbp:propulsion
|
11.67
approximately 3,500 lbf
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:services
|
1980
approximately 5,000 hours
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:supportRole
|
pilot training
light attack missions
|
|
gptkbp:supports
|
ground support equipment available
|
|
gptkbp:usedIn
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:weight
|
approximately 300 kg
|