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gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:controls
|
digital control system
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:designedFor
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:engine
|
75 dB
intercooler
pylon-mounted
air starter
|
|
gptkbp:engineConfiguration
|
twin-spool
low-bypass ratio
|
|
gptkbp:engineDisplacement
|
modular design
|
|
gptkbp:engineType
|
high reliability
turbojet
axial
single-stage
high fuel efficiency
high thrust-to-weight ratio
high thermal efficiency
low maintenance requirements
|
|
gptkbp:fanBase
|
single-stage fan
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuel_capacity
|
0.5 kg/s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
spark plug
|
|
gptkbp:hasArea
|
gptkb:Rolls-Royce_test_facility
static testing
|
|
gptkbp:hasContent
|
0.8 lb/hp/hr
|
|
gptkbp:hasDepartment
|
no
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 3400
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:maxSpeed
|
Mach_0.9
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
|
|
gptkbp:numberOfEpisodes
|
1
|
|
gptkbp:operationalArea
|
gptkb:Royal_Air_Force
|
|
gptkbp:operationalRange
|
2000 km
|
|
gptkbp:operationalStatus
|
up to 40,000 ft
|
|
gptkbp:performances
|
3000 hours
|
|
gptkbp:producedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:propulsion
|
22.67
3400 lbf
|
|
gptkbp:related_engine
|
brayton_cycle
|
|
gptkbp:services
|
1976
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:updates
|
upgradable to Mk 951
|
|
gptkbp:weight
|
150 kg
|