|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:airlines
|
30 kg/s
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:climate
|
1500 K
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
interstage cooling
|
|
gptkbp:design
|
5000 hours
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
CAA
|
|
gptkbp:engineConfiguration
|
twin-shaft
|
|
gptkbp:engineType
|
axial
single_spool
|
|
gptkbp:exportedTo
|
multiple countries
|
|
gptkbp:fanBase
|
single stage fan
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:firstRace
|
1964
|
|
gptkbp:fuel_capacity
|
high efficiency
0.8 lb/hp/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
gptkbp:historicalEvent
|
derived_from_the_Rolls-Royce_Spey
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 900
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:market_segment
|
trainer aircraft
|
|
gptkbp:modifications
|
upgraded to Mk 951
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
|
|
gptkbp:number_of_stages
|
8
|
|
gptkbp:operational_status
|
in production
|
|
gptkbp:operationalRange
|
1,000 km
|
|
gptkbp:propulsion
|
6:1
9000 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_951
gptkb:Adour_Mk_1000
gptkb:Adour_Mk_871
Brayton_cycle
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:reviews
|
excellent performance
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:training
|
joint_development_with_British_Aerospace
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
1500 lb
|