Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbofan engine
|
| gptkbp:application |
military training aircraft
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:designedFor |
gptkb:Hawker_Siddeley_Hawk
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:engineConfiguration |
twin-spool
|
| gptkbp:engineType |
turbojet
axial single-stage |
| gptkbp:firstFlight |
1974
|
| gptkbp:fuelType |
gptkb:Jet_A-1
|
| gptkbp:hasContent |
0.8 lb/hp/hr
|
| https://www.w3.org/2000/01/rdf-schema#label |
Adour Mk 2300
|
| gptkbp:length |
1.5 m
|
| gptkbp:maxSpeed |
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:producedBy |
gptkb:Rolls-Royce
|
| gptkbp:propulsion |
2300 lbf
|
| gptkbp:status |
in service
|
| gptkbp:weight |
150 kg
|