|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:airlines
|
30 kg/s
|
|
gptkbp:application
|
trainer aircraft
|
|
gptkbp:component
|
aluminum
steel
composite materials
titanium
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:debutYear
|
1974
|
|
gptkbp:design
|
modular design
high thrust-to-weight ratio
training and light attack
low maintenance requirements
versatile application
|
|
gptkbp:designedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
CAA
|
|
gptkbp:energyEfficiency
|
high
|
|
gptkbp:engine
|
Adour_family
|
|
gptkbp:engineConfiguration
|
twin-shaft
|
|
gptkbp:engineType
|
axial
single_spool
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
gptkbp:hasContent
|
0.8 lb/hp/hr
|
|
gptkbp:historicalEvent
|
derived_from_Adour_Mk_100
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 2100
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:maximumDepth
|
1500 K
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
|
|
gptkbp:numberOfStudents
|
5
|
|
gptkbp:operationalArea
|
military training
|
|
gptkbp:operationalStatus
|
in service
|
|
gptkbp:propulsion
|
8.4
2100 lbf
|
|
gptkbp:related_engine
|
brayton_cycle
|
|
gptkbp:reliability
|
high
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
military engine
|
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:weight
|
250 kg
|