|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
compatible with various aircraft
Hawk_family
|
|
gptkbp:application
|
trainer aircraft
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:design
|
modular design
training and light attack missions
|
|
gptkbp:designedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:developer
|
developed_from_Adour_Mk_100
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
compliant_with_ICAO_standards
|
|
gptkbp:energyEfficiency
|
high fuel efficiency
|
|
gptkbp:engine
|
250 kg
air start
pylon-mounted
|
|
gptkbp:engineConfiguration
|
twin-shaft
twin-shaft configuration
|
|
gptkbp:engineType
|
turbojet
axial
good performance at altitude
single_spool
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelCapacity
|
0.8 kg/s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
gptkbp:hasArea
|
extensively tested
|
|
gptkbp:hasDepartment
|
no
|
|
gptkbp:hasFieldOfUse
|
gptkb:BAE_Systems_Hawk
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 3700
|
|
gptkbp:legacy
|
successor to earlier designs.
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_plc
|
|
gptkbp:marketSegment
|
military aviation
|
|
gptkbp:maximumDepth
|
12,000 m
3700 lbf
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operationalArea
|
used in training roles
|
|
gptkbp:operationalHistory
|
used by several air forces
|
|
gptkbp:performances
|
3000 hours
|
|
gptkbp:propulsion
|
14.8
3700 lbf
|
|
gptkbp:related_engine
|
brayton_cycle
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:services
|
1976
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
military engine
|
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:weight
|
250 kg
|