Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:cycle |
turbofan
|
| gptkbp:derivedFrom |
gptkb:Saturn_AL-31F
|
| gptkbp:diameter |
0.905 m
|
| gptkbp:firstFlight |
1990s
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Saturn AL-31FN
|
| gptkbp:intendedUse |
single-engine fighter aircraft
|
| gptkbp:length |
4.95 m
|
| gptkbp:manufacturer |
gptkb:NPO_Saturn
|
| gptkbp:notableClient |
gptkb:China
|
| gptkbp:notableFeature |
modified gearbox for under-fuselage mounting
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
12,500 kgf
7,800 kgf |
| gptkbp:usedIn |
gptkb:Chengdu_J-20_(early_prototypes)
gptkb:Chengdu_J-10 |
| gptkbp:weight |
1,520 kg
|
| gptkbp:bfsParent |
gptkb:Chengdu_J-10
|
| gptkbp:bfsLayer |
6
|