Statements (16)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:China
|
| gptkbp:developedBy |
gptkb:China
|
| gptkbp:firstFlight |
early 2000s
|
| https://www.w3.org/2000/01/rdf-schema#label |
WS-10A
|
| gptkbp:manufacturer |
gptkb:Shenyang_Aeroengine_Research_Institute
|
| gptkbp:primaryUser |
gptkb:People's_Liberation_Army_Air_Force
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
approximately 13,200 kgf (with afterburner)
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:Chengdu_J-10
gptkb:Shenyang_J-11 gptkb:Shenyang_J-16 |
| gptkbp:bfsParent |
gptkb:WS-10B
gptkb:WS-10C |
| gptkbp:bfsLayer |
7
|