gptkbp:instanceOf
|
jet engine
|
gptkbp:application
|
military training aircraft
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
gptkbp:coolingSystem
|
air-cooled
water-glycol
|
gptkbp:design_feature
|
compact design
|
gptkbp:developer
|
developed_from_Adour_Mk_871
|
gptkbp:diameter
|
0.9 m
|
gptkbp:emissionsStandard
|
complies with international standards
|
gptkbp:engine
|
modular
inline
|
gptkbp:engineConfiguration
|
twin-spool
|
gptkbp:engineType
|
axial
air start
single-stage high-pressure turbine
|
gptkbp:environmentalProtection
|
meets noise regulations
|
gptkbp:exhaustSystem
|
straight
subsonic
|
gptkbp:firstFlight
|
1974
|
gptkbp:fuel_capacity
|
high efficiency
0.8 kg/kN·h
1,200 kg/h
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
dual fuel system
|
gptkbp:hasArea
|
static and flight testing
|
gptkbp:hasDepartment
|
no
|
gptkbp:historicalEvent
|
evolved from earlier models
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 871-31K-12D-19
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
gptkbp:keyIssues
|
various air forces worldwide
|
gptkbp:length
|
1.8 m
|
gptkbp:maintenance
|
1,000 hours
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
gptkbp:market_segment
|
military aviation
|
gptkbp:noise_level
|
low noise emissions
|
gptkbp:notable_feature
|
Adour_Mk_871-31K-12D-19A
Adour_Mk_871-31K-12D-19B
|
gptkbp:operational_status
|
gptkb:Royal_Air_Force
multi-role capability
|
gptkbp:operationalHistory
|
used in various air forces
|
gptkbp:operationalRange
|
1,500 km
|
gptkbp:performance
|
high thrust-to-weight ratio
|
gptkbp:performances
|
approximately 5,000 hours
|
gptkbp:propulsion
|
no
approximately 3,500 lbf
|
gptkbp:providesServices
|
comprehensive maintenance support
|
gptkbp:related_engine
|
gptkb:Adour_Mk_871
Adour_Mk_871-31K-12D-19C
|
gptkbp:safety_features
|
over-speed protection
|
gptkbp:service_ceiling
|
12,000 m
|
gptkbp:training
|
integrated training systems
|
gptkbp:type
|
turbofan engine
|
gptkbp:weight
|
approximately 300 kg
|