|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
Hawk_family
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:developer
|
gptkb:Rolls-Royce
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:emissionsStandard
|
compliant_with_ICAO
|
|
gptkbp:engine
|
various applications
state-of-the-art technology
modern design
modular
rear-mounted
advanced trainer aircraft
|
|
gptkbp:engineConfiguration
|
mass production
twin-spool
military aviation market
|
|
gptkbp:engineType
|
axial
single-stage
advanced features
multiple variants
air start
Mk 871-31L10 variant
|
|
gptkbp:exhaustSystem
|
variable geometry
|
|
gptkbp:firstFlight
|
1970s
|
|
gptkbp:fuel_capacity
|
1,200 lb/hr
0.8 lb/hp/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
hydromechanical
|
|
gptkbp:hasArea
|
ground testing
EASA_certified
|
|
gptkbp:hasDepartment
|
no
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 871-31L10
|
|
gptkbp:is_used_in
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:number_of_stages
|
8
|
|
gptkbp:operational_status
|
gptkb:Royal_Air_Force
|
|
gptkbp:operationalRange
|
1,000 km
up to 40,000 ft
|
|
gptkbp:performances
|
high performance
high reliability
detailed specifications
|
|
gptkbp:propulsion
|
11.7
approximately 3,500 lbf
11.7 lbf/lb
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_871
Brayton_cycle
|
|
gptkbp:serviceType
|
1980s
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 300 kg
|