Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:countryOfOrigin |
gptkb:China
|
| gptkbp:firstFlight |
2010s
|
| gptkbp:improves |
gptkb:WS-10B
|
| gptkbp:manufacturer |
gptkb:Shenyang_Aeroengine_Research_Institute
|
| gptkbp:notableFeature |
improved reliability
higher thrust |
| gptkbp:relatedTo |
gptkb:WS-10A
gptkb:WS-10 gptkb:WS-10B |
| gptkbp:status |
in service
|
| gptkbp:thrust |
approximately 142 kN
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedInAircraft |
gptkb:Shenyang_J-11B
gptkb:Chengdu_J-20 gptkb:Shenyang_J-16 |
| gptkbp:bfsParent |
gptkb:Chengdu_J-20
gptkb:J-20_Mighty_Dragon gptkb:J-20_stealth_fighter |
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
WS-10C
|