Responsibilities:

1, responsible for the main structure of the launch vehicle, institutional product program demonstration, design, drawing, acceptance and follow-up work;

2, responsible for the launch vehicle assembly design, drawing and production work;

3, responsible for the launch vehicle structure, institutional functional test and other tasks, test outline;

4. Responsible for flight test of structural system products.

Requirements:

1. Master degree or above in aircraft general design, aircraft manufacturing, mechanical design and manufacturing, mechanics and other related majors;

2, skilled use of structural design related software, skilled use of kinematics, dynamics and other related analysis software.