Statements (51)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
jet engine
|
| gptkbp:application |
advanced jet trainer
military training aircraft |
| gptkbp:competitors |
other turbofan engines
|
| gptkbp:controls |
digital control system
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:design_feature |
advanced aerodynamics
enhanced performance lightweight materials modular design state-of-the-art technology environmentally friendly design increased durability high bypass ratio reduced drag modular maintenance advanced materials technology improved thrust vectoring simplified assembly |
| gptkbp:developer |
gptkb:joint_venture_between_Rolls-Royce_and_British_Aerospace
|
| gptkbp:diameter |
approximately 0.9 m
|
| gptkbp:emissionsStandard |
compliant with regulations
|
| gptkbp:engineType |
axial compressor
single-stage turbine |
| gptkbp:firstRace |
1960s
|
| gptkbp:fuel_capacity |
good fuel efficiency
|
| gptkbp:fuelType |
gptkb:Jet_A-1
annular combustor |
| https://www.w3.org/2000/01/rdf-schema#label |
Adour Mk 33000
|
| gptkbp:is_used_in |
gptkb:Hawker_Siddeley_Hawk
|
| gptkbp:length |
approximately 1.5 m
|
| gptkbp:maintenance |
low maintenance requirements
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:market |
military aviation market
|
| gptkbp:noise_level |
low noise design
|
| 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 stages
|
| gptkbp:operationalRange |
up to 40,000 feet
up to 90% of maximum thrust |
| gptkbp:propulsion |
10:1
approximately 3,000 lbf |
| gptkbp:reliability |
high reliability
|
| gptkbp:serviceType |
1976
|
| gptkbp:successor |
gptkb:Adour_Mk_951
|
| gptkbp:type |
turbofan engine
|
| gptkbp:variant |
gptkb:Adour_Mk_871
|
| gptkbp:weight |
approximately 300 kg
|