The Guizhou WS-19, code name Huangshan, is an afterburner turbofan engine designed by the Guizhou Aeroengine Design
Institute. It has a reported thrust-to-weight ratio of 10 and a thrust of 10 metric tons or 22,000 lbs.
Design
The reported maximum thrust of the WS-19 is . ==Specifications (WS-19)==