|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
Hawk_family
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:controls
|
digital control system
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:designedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:developer
|
Rolls-Royce Adour
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
low emissions
|
|
gptkbp:engine
|
advanced technology
intercooler
various military aircraft
detailed specifications available
fuselage-mounted
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
high performance
high reliability
turbojet engine
long lifespan
axial compressor
single-stage turbine
certified by authorities
|
|
gptkbp:firstFlight
|
1970s
|
|
gptkbp:fuelCapacity
|
0.8 kg/s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
|
|
gptkbp:hasArea
|
ground testing
|
|
gptkbp:hasDepartment
|
no
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 951
|
|
gptkbp:introduced
|
1980s
|
|
gptkbp:launchSite
|
starter motor
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maxSpeed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operationalRange
|
1,000 km
|
|
gptkbp:operationalStatus
|
in service
|
|
gptkbp:propulsion
|
no
approximately 4,000 lbf
|
|
gptkbp:related_engine
|
brayton_cycle
|
|
gptkbp:relatedPatent
|
gptkb:Adour_Mk_871
|
|
gptkbp:replacedBy
|
gptkb:Adour_Mk_951R
|
|
gptkbp:services
|
12,000 m
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951R
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:updates
|
possible upgrades
|
|
gptkbp:usedIn
|
gptkb:BAE_Systems_Hawk
gptkb:McDonnell_Douglas_T-45_Goshawk
|
|
gptkbp:variant
|
gptkb:Adour_Mk_951R
|
|
gptkbp:weight
|
approximately 300 kg
|