|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:application
|
trainer aircraft
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:design
|
modular design
|
|
gptkbp:designedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engine
|
1.5 m
400 kg
air-cooled
pylon-mounted
air-start
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineDisplacement
|
0.9 m
|
|
gptkbp:enginePower
|
4,000 lbf
|
|
gptkbp:engineType
|
turbojet
axial
single-stage
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelCapacity
|
0.5 kg/kN/h
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 4100
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maxSpeed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
|
|
gptkbp:numberOfStudents
|
8
|
|
gptkbp:operationalArea
|
military training
|
|
gptkbp:operationalStatus
|
up to 40,000 ft
|
|
gptkbp:propulsion
|
10:1
approximately 4,000 lbf
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:relatedTo
|
gptkb:Adour_engine_family
|
|
gptkbp:services
|
1976
|
|
gptkbp:successor
|
gptkb:Adour_Mk_811
|
|
gptkbp:type
|
military engine
|
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:weight
|
approximately 400 kg
|