|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
Hawk_family
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:designedFor
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:developer
|
jointly_developed_by_Rolls-Royce_and_Turbomeca
|
|
gptkbp:diameter
|
approximately 0.9 m
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engine
|
gptkb:Adour_Mk_4900
1.5 m
1,200 lb
air start
pylon-mounted
military training and light attack
|
|
gptkbp:engineConfiguration
|
gptkb:Rolls-Royce
single-engine
|
|
gptkbp:engineDisplacement
|
0.9 m
|
|
gptkbp:enginePower
|
4,000 lbf
|
|
gptkbp:engineType
|
turbojet
axial
high-pressure and low-pressure turbines
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelCapacity
|
approximately 0.8 kg/s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 4900
|
|
gptkbp:length
|
approximately 1.5 m
|
|
gptkbp:maintenance
|
approximately 1,000 hours
|
|
gptkbp:noise_level
|
compliant_with_ICAO_standards
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
|
|
gptkbp:numberOfStudents
|
8
|
|
gptkbp:operationalArea
|
training and light attack missions
|
|
gptkbp:operationalStatus
|
up to 40,000 ft
|
|
gptkbp:producedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:propulsion
|
3.33
approximately 4,000 lbf
|
|
gptkbp:relatedPatent
|
gptkb:Adour_Mk_951
gptkb:Adour_Mk_1000
gptkb:Adour_Mk_871
|
|
gptkbp:services
|
1976
|
|
gptkbp:setting
|
twin-spool
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:totalGoals
|
over 1,000 units
|
|
gptkbp:weight
|
approximately 1,200 lb
|