Statements (29)
| 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:coolingSystem |
air-cooled
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:engineType |
axial
single-stage high-pressure turbine |
| gptkbp:fuel_capacity |
0.8 lb/hp/hr
|
| gptkbp:fuelType |
gptkb:Jet_A-1
annular |
| https://www.w3.org/2000/01/rdf-schema#label |
Adour Mk 42000
|
| gptkbp:introduced |
1970s
|
| gptkbp:is_used_in |
gptkb:Hawker_Siddeley_Hawk
|
| gptkbp:length |
1.8 m
|
| gptkbp:maintenance |
200 hours
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:maximum_speed |
Mach_0.9
|
| 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 30,000 ft
|
| gptkbp:propulsion |
4200 lbf
|
| gptkbp:related_engine |
two-spool
|
| gptkbp:successor |
gptkb:Adour_Mk_871
|
| gptkbp:type |
turbofan engine
|
| gptkbp:weight |
approximately 400 kg
|