Statements (33)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
gptkb:trainer_aircraft |
| gptkbp:countryOfOrigin |
gptkb:France
gptkb:United_Kingdom |
| gptkbp:developedBy |
gptkb:SEPECAT_Jaguar
|
| gptkbp:diameter |
0.72 m
|
| gptkbp:firstRun |
1968
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Turbomeca Adour
|
| gptkbp:length |
2.9 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
gptkb:Turbomeca |
| gptkbp:militaryDesignation |
gptkb:F405-RR-401
gptkb:F405-RR-402 |
| gptkbp:notableFeature |
modular design
afterburning and non-afterburning variants low bypass ratio |
| gptkbp:status |
in production
|
| gptkbp:thrust |
up to 8,430 lbf (37.5 kN)
|
| gptkbp:type |
twin-spool turbofan
|
| gptkbp:usedIn |
gptkb:McDonnell_Douglas_T-45_Goshawk
gptkb:SEPECAT_Jaguar gptkb:BAE_Systems_Hawk gptkb:HAL_Tejas_(trainer_variant) |
| gptkbp:variant |
gptkb:Adour_Mk_101
gptkb:Adour_Mk_102 gptkb:Adour_Mk_104 gptkb:Adour_Mk_106 gptkb:Adour_Mk_871 gptkb:Adour_Mk_811 gptkb:Adour_Mk_951 |
| gptkbp:bfsParent |
gptkb:BAE_Hawk
|
| gptkbp:bfsLayer |
5
|