Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:constructionStartYear |
early 2000s
|
| gptkbp:countryOfOrigin |
gptkb:China
|
| gptkbp:diameter |
1.7 m
|
| gptkbp:firstFlight |
2013
|
| https://www.w3.org/2000/01/rdf-schema#label |
WS-20
|
| gptkbp:length |
5.5 m
|
| gptkbp:manufacturer |
gptkb:Shenyang_Aeroengine_Research_Institute
|
| gptkbp:primaryUser |
gptkb:People's_Liberation_Army_Air_Force
|
| gptkbp:relatedTo |
gptkb:WS-10
|
| gptkbp:replacedBy |
gptkb:Soloviev_D-30KP-2
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
138 kN
|
| gptkbp:type |
high-bypass turbofan
|
| gptkbp:usedInAircraft |
gptkb:Xian_Y-20
|
| gptkbp:weight |
2,500 kg
|
| gptkbp:bfsParent |
gptkb:Xian_Y-20
|
| gptkbp:bfsLayer |
6
|