Statements (23)
Predicate | Object |
---|---|
gptkbp:instanceOf |
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
|
https://www.w3.org/2000/01/rdf-schema#label |
WS-10B
|
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
|