|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
Hawk_family
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:controls
|
digital
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:designedFor
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
low
|
|
gptkbp:energyEfficiency
|
high
|
|
gptkbp:engine
|
1.5 m
classified
200 kg
military and civilian
wing-mounted
air start
afterburner
advanced trainer aircraft
3200 lbf
|
|
gptkbp:engineConfiguration
|
turbojet
single-engine
|
|
gptkbp:engineDisplacement
|
0.9 m
ongoing
|
|
gptkbp:engineType
|
gptkb:Jet_A-1
gptkb:Adour_Mk_100
turbofan
air-cooled
axial
reliable
single_spool
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelCapacity
|
0.5 kg/s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
spark plug
|
|
gptkbp:hasArea
|
ground testing
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 3200
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
100 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_plc
|
|
gptkbp:maxSpeed
|
Mach_0.9
|
|
gptkbp:noise_level
|
85 dB
|
|
gptkbp:numberOfEpisodes
|
1
|
|
gptkbp:operationalHistory
|
developed_in_the_UK
|
|
gptkbp:operationalRange
|
2000 km
|
|
gptkbp:operationalStatus
|
12,000 m
|
|
gptkbp:performances
|
5000 hours
|
|
gptkbp:producedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:propulsion
|
no
16:1
3200 lbf
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:services
|
1976
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:usedIn
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:weight
|
200 kg
|