|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:design
|
modular construction
|
|
gptkbp:designedFor
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
compliant_with_ICAO
|
|
gptkbp:engine
|
pylon-mounted
air-start
|
|
gptkbp:engineConfiguration
|
single-spool
|
|
gptkbp:engineType
|
turbojet
axial
single-stage
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelCapacity
|
1,200 lb/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
gptkbp:hasArea
|
extensive ground testing
|
|
gptkbp:hasCompetitors
|
Pratt & Whitney JT15D
|
|
gptkbp:hasContent
|
0.8 lb/hp/hr
|
|
gptkbp:historicalSignificance
|
used in various military aircraft.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 35000
|
|
gptkbp:introduced
|
1974
|
|
gptkbp:lastProduced
|
1972
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:maxSpeed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:numberOfStudents
|
8
|
|
gptkbp:operationalArea
|
training and light attack missions
|
|
gptkbp:operationalRange
|
up to 30,000 ft
|
|
gptkbp:performances
|
3,000 hours
|
|
gptkbp:producedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:productionCompany
|
1968
|
|
gptkbp:propulsion
|
not available
11:1
around 3,500 lbf
|
|
gptkbp:relatedTo
|
gptkb:Adour_Mk_951
|
|
gptkbp:replacedBy
|
gptkb:Adour_Mk_951
|
|
gptkbp:services
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:totalGoals
|
over 1,000 units
|
|
gptkbp:usedBy
|
gptkb:Royal_Air_Force
|
|
gptkbp:usedIn
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:weight
|
around 300 kg
|