Statements (24)
| 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 3 ft
|
| gptkbp:engineConfiguration |
twin-spool
|
| gptkbp:engineType |
axial compressor
axial turbine |
| gptkbp:fuelType |
gptkb:Jet_A-1
afterburning |
| https://www.w3.org/2000/01/rdf-schema#label |
Adour Mk 871-31L21
|
| gptkbp:introduced |
1970s
|
| gptkbp:is_used_in |
gptkb:Hawker_Siddeley_Hawk
|
| gptkbp:length |
approximately 12 ft
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notable_feature |
gptkb:Adour_Mk_871
|
| gptkbp:operational_status |
training and light attack missions
|
| gptkbp:origin |
gptkb:United_Kingdom
|
| gptkbp:propulsion |
approximately 3,500 lbf
|
| gptkbp:related_engine |
gptkb:Adour_Mk_951
|
| gptkbp:successor |
gptkb:Adour_Mk_951
|
| gptkbp:type |
turbofan engine
|
| gptkbp:weight |
approximately 1,200 lb
|