|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
Hawk_family
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
gptkb:United_Kingdom
|
|
gptkbp:designedFor
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
low
|
|
gptkbp:engine
|
low
1.5 m
150 kg
air start
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineDisplacement
|
0.9 m
|
|
gptkbp:engineType
|
air-cooled
axial
single-stage
afterburning turbofan
200 hours
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelCapacity
|
0.5 kg/s
|
|
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 2400
|
|
gptkbp:launchSite
|
air start
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_plc
|
|
gptkbp:maximumDepth
|
2400 lbf
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operationalArea
|
training and light attack missions
|
|
gptkbp:operationalRange
|
high subsonic speeds
|
|
gptkbp:producedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:propulsion
|
16:1
2400 lbf
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:relatedPatent
|
gptkb:Adour_Mk_951
|
|
gptkbp:services
|
1976
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbojet engine
|
|
gptkbp:usedIn
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:weight
|
150 kg
|