Abstract：In order to improve the available overload and fast overload response of air defense missile, the application of trajectory-controlled thrust vector technology in foreign air defense missiles is analyzed．The method of matching design of trajectory-controlled thrust vector device and missile shape is studied by using jet disturbance factor．The method of moment balance iteration is used to design the action point of trajectory-controlled thrust and the arrangement of missile center of gravity．The influence of trajectory-controlled thrust vector device on the load, strength and overload characteristics of missile is analyzed and the corresponding measures are put forward．
管再升, 阮文华, 刘伟, 施振兴, 李欣益. 轨控推力矢量技术在防空导弹上的应用研究[J]. 空天防御, 2020, 3(2): 1-7.
GUAN Zaisheng, RUAN Wenhua, LIU Wei, SHI Zhenxing, LI Xinyi. Study of Trajectory-controlled Thrust Vector Technology Application in Air Defense Missile. Air & Space Defense, 2020, 3(2): 1-7.
