|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
Hawk_family
|
|
gptkbp:application
|
trainer aircraft
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:designedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
CAA
|
|
gptkbp:energyEfficiency
|
high
|
|
gptkbp:engine
|
1.5 m
250 kg
air start
pylon-mounted
|
|
gptkbp:engineConfiguration
|
twin-shaft
|
|
gptkbp:engineDisplacement
|
0.9 m
|
|
gptkbp:enginePower
|
3100 lbf
|
|
gptkbp:engineType
|
turbojet
axial
single_spool
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
gptkbp:hasContent
|
0.8 lb/hp/hr
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 3100
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximumDepth
|
12000 m
|
|
gptkbp:maxSpeed
|
0.9 Mach
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:numberBuilt
|
over 1000
|
|
gptkbp:operationalArea
|
military training
|
|
gptkbp:operationalRange
|
2000 km
|
|
gptkbp:performances
|
5000 hours
|
|
gptkbp:propulsion
|
12.4
3100 lbf
|
|
gptkbp:related_engine
|
brayton_cycle
|
|
gptkbp:relatedPatent
|
gptkb:Adour_Mk_951
|
|
gptkbp:services
|
1976
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
military engine
|
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:weight
|
250 kg
|