gptkbp:instanceOf
|
jet engine
|
gptkbp:aircraft
|
Hawk_family
|
gptkbp:application
|
military training aircraft
|
gptkbp:controls
|
FADEC
|
gptkbp:coolingSystem
|
air-cooled
|
gptkbp:designedBy
|
gptkb:Rolls-Royce
|
gptkbp:diameter
|
0.9 m
|
gptkbp:emissionsStandard
|
low
|
gptkbp:engine
|
1.5 m
1,500 kg
pylon-mounted
|
gptkbp:engineConfiguration
|
twin-spool
|
gptkbp:engineDisplacement
|
0.9 m
|
gptkbp:engineType
|
turbojet
axial
single-stage
|
gptkbp:firstFlight
|
1974
|
gptkbp:fuelCapacity
|
0.8 kg/s
|
gptkbp:fuelType
|
gptkb:Jet_A-1
spark ignition
|
gptkbp:hasDepartment
|
no
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 39000
|
gptkbp:launchSite
|
air starter
|
gptkbp:length
|
1.5 m
|
gptkbp:maintenance
|
1,000 hours
|
gptkbp:maxSpeed
|
0.9 Mach
|
gptkbp:noise_level
|
low
|
gptkbp:operationalArea
|
gptkb:United_Arab_Emirates_Air_Force
gptkb:Australian_Air_Force
gptkb:Singapore_Air_Force
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Navy
gptkb:Kuwaiti_Air_Force
gptkb:Royal_Malaysian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
|
gptkbp:producedBy
|
gptkb:Rolls-Royce
|
gptkbp:propulsion
|
26:1
3900 lbf
|
gptkbp:range
|
1,500 km
|
gptkbp:services
|
15,000 m
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
gptkbp:type
|
turbofan engine
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
|
gptkbp:weight
|
150 kg
|