Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
jet engine
|
| gptkbp:aircraft |
gptkb:BAE_Systems_Hawk
|
| gptkbp:application |
military training aircraft
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
approximately 0.9 m
|
| gptkbp:emissionsStandard |
compliant_with_ICAO_standards
|
| gptkbp:engineType |
single-stage axial compressor
single-stage axial turbine |
| gptkbp:fanBase |
single-stage fan
|
| gptkbp:fuel_capacity |
0.8 lb/hp/hr
|
| gptkbp:fuelType |
gptkb:Jet_A-1
annular combustor |
| https://www.w3.org/2000/01/rdf-schema#label |
Adour Mk 871-31L11A
|
| gptkbp:introduced |
1970s
|
| gptkbp:is_used_in |
gptkb:Hawker_Siddeley_Hawk
|
| gptkbp:length |
approximately 1.5 m
|
| gptkbp:maintenance |
1,000 hours
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:noise_level |
low noise
|
| gptkbp:operationalRange |
up to 30,000 ft
|
| gptkbp:propulsion |
approximately 3,500 lbf
|
| gptkbp:successor |
gptkb:Adour_Mk_951
|
| gptkbp:type |
turbofan engine
|
| gptkbp:weight |
approximately 400 lb
|