Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbofan engine
|
| gptkbp:application |
advanced jet trainer
military training aircraft |
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:design |
twin-spool
|
| gptkbp:diameter |
800 mm
|
| gptkbp:emissionsStandard |
compliant_with_ICAO_standards
|
| gptkbp:engineType |
axial compressor
high-pressure turbine |
| gptkbp:fuelType |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Adour Mk 245
|
| gptkbp:introduced |
1980s
|
| gptkbp:is_used_in |
gptkb:BAE_Systems_Hawk
|
| gptkbp:length |
1,800 mm
|
| gptkbp:maintenance |
1,500 hours
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:noise_level |
low noise
|
| gptkbp:number_of_stages |
10 stages
|
| gptkbp:operationalRange |
varied by aircraft
|
| gptkbp:origin |
gptkb:United_Kingdom
|
| gptkbp:performance |
high thrust-to-weight ratio
|
| gptkbp:propulsion |
approximately 4,000 lbf
|
| gptkbp:related_engine |
brayton_cycle
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:Adour_Mk_951
|
| gptkbp:weight |
approximately 300 kg
|