Description

The Kunlun series of turbine engines represents a significant advancement in aerospace technology, featuring an axial flow type double rotor engine with an afterburner turbojet design. As China’s first engine developed under the comprehensive implementation of GJB standards, the Kunlun engine showcases the country’s commitment to self-reliance in aviation technology. With 18 years of dedicated research and development, it has successfully addressed numerous technical challenges, refining its performance through extensive ground and air testing. The design was officially approved on July 10, 2002, marking a milestone in China’s aviation capabilities.

Specifications