Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
military fighter aircraft
|
| gptkbp:category |
military aircraft engine
|
| gptkbp:countryOfOrigin |
gptkb:China
|
| gptkbp:diameter |
1.3 m
|
| gptkbp:enteredService |
2010s
|
| gptkbp:firstFlight |
2002
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:improves |
gptkb:WS-10A
|
| gptkbp:length |
4.8 m
|
| gptkbp:manufacturer |
gptkb:Shenyang_Aeroengine_Research_Institute
|
| gptkbp:relatedTo |
gptkb:WS-10A
gptkb:WS-10 |
| gptkbp:thrust |
approximately 13,200 kgf (with afterburner)
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedInAircraft |
gptkb:Shenyang_J-20
gptkb:Chengdu_J-10 gptkb:Shenyang_J-11 gptkb:Shenyang_J-16 |
| gptkbp:weight |
1,600 kg
|
| gptkbp:bfsParent |
gptkb:J-10C
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
WS-10B
|