Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
jet engine
|
| gptkbp:aircraft |
Hawk_family
|
| gptkbp:application |
military training aircraft
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:diameter |
approximately 0.9 m
|
| gptkbp:engineType |
axial
single-stage high-pressure turbine |
| gptkbp:firstRace |
1970s
|
| gptkbp:fuelType |
gptkb:Jet_A-1
annular |
| https://www.w3.org/2000/01/rdf-schema#label |
Adour Mk 871-31L1
|
| gptkbp:is_used_in |
gptkb:Hawker_Siddeley_Hawk
|
| gptkbp:length |
approximately 1.5 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| 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 1,200 lb
|