Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:afterburning |
yes
|
| gptkbp:constructionStartYear |
1990s
|
| gptkbp:countryOfOrigin |
gptkb:China
|
| gptkbp:designation |
Turbofan-15
|
| gptkbp:diameter |
approximately 1 meter
|
| gptkbp:features |
thrust vectoring
supercruise capability |
| gptkbp:firstFlight |
2022
|
| gptkbp:generation |
fourth-generation turbofan
|
| https://www.w3.org/2000/01/rdf-schema#label |
WS-15 engine
|
| gptkbp:intendedUse |
fifth-generation fighter aircraft
|
| gptkbp:length |
approximately 5 meters
|
| gptkbp:manufacturer |
gptkb:Shenyang_Aeroengine_Research_Institute
|
| gptkbp:maximumSpeed |
180 kN
|
| gptkbp:replacedBy |
WS-10 engine
|
| gptkbp:status |
in testing
|
| gptkbp:thrust |
18 tons
|
| gptkbp:type |
low-bypass turbofan
|
| gptkbp:usedIn |
gptkb:Chengdu_J-20
|
| gptkbp:weight |
approximately 1800 kg
|
| gptkbp:bfsParent |
gptkb:J-20_fighter_jet
|
| gptkbp:bfsLayer |
6
|