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gptkbp:instanceOf
|
turbojet engine
|
|
gptkbp:aircraft
|
multiple aircraft types
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|
gptkbp:application
|
military training aircraft
|
|
gptkbp:controls
|
FADEC
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|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
Euro I
|
|
gptkbp:engine
|
inline
|
|
gptkbp:engineConfiguration
|
ongoing
twin-spool
military and civilian
|
|
gptkbp:engineType
|
turbojet
axial
air start
1,500 °C
single_spool
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuel_capacity
|
moderate
0.85 lb/hp/hr
0.5 kg/s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
gptkbp:hasArea
|
gptkb:Derby,_UK
completed in 1974
conducted_at_Rolls-Royce
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 151
|
|
gptkbp:inspiration
|
training and light attack
|
|
gptkbp:introduced
|
1974
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
3.4 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:market
|
good
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low
achieved through design
|
|
gptkbp:notable_feature
|
Adour Mk 151-1
|
|
gptkbp:operational_status
|
gptkb:Royal_Air_Force
|
|
gptkbp:operationalRange
|
1,500 km
|
|
gptkbp:origin
|
gptkb:United_Kingdom
|
|
gptkbp:performances
|
high
3,000 hours
high thrust-to-weight ratio
available online.
every 1,500 hours
|
|
gptkbp:propulsion
|
not available
3,500 lbf
8.75:1
|
|
gptkbp:related_engine
|
Brayton_cycle
Rolls-Royce_engineers
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
afterburning turbojet engine
|
|
gptkbp:updates
|
available for military applications
|
|
gptkbp:warranty
|
2 years or 1,000 hours
|
|
gptkbp:weight
|
400 kg
|