Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbofan engine
|
| gptkbp:aircraft |
trainer aircraft
|
| gptkbp:application |
military training
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
approximately 0.9 m
|
| gptkbp:engineConfiguration |
twin-spool
|
| gptkbp:engineType |
axial compressor
single-stage turbine |
| gptkbp:fanBase |
single-stage fan
|
| gptkbp:fuel_capacity |
0.8 kg/lbf/h
|
| gptkbp:fuelType |
gptkb:Jet_A-1
annular |
| https://www.w3.org/2000/01/rdf-schema#label |
Adour Mk 171-40E
|
| gptkbp:introduced |
1970s
|
| gptkbp:is_used_in |
gptkb:Hawker_Siddeley_Hawk
|
| gptkbp:length |
approximately 1.5 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| 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:operationalRange |
up to 1,000 km
|
| gptkbp:propulsion |
approximately 3,500 lbf
|
| gptkbp:service_ceiling |
12,000 m
|
| gptkbp:successor |
gptkb:Adour_Mk_151
|
| gptkbp:type |
military engine
|
| gptkbp:weight |
approximately 300 kg
|