Welcome to Acta Armamentarii ! Today is

Acta Armamentarii ›› 2025, Vol. 46 ›› Issue (9): 241006-.doi: 10.12382/bgxb.2024.1006

Previous Articles     Next Articles

Failure Mechanism of Solder Joints of Projectile-borne Electronic Package under High Overload Environment

LIU Qiming, FAN Zhengyan, LI Tao, YANG Weilong, HAN Xu*()   

  1. School of Mechanical Engineering, Hebei University of Technology, Tianjin 300401, China
  • Received:2024-11-05 Online:2025-09-24
  • Contact: HAN Xu

Abstract:

As an important part of control system for a guided projectile,the solder joints of projectile-borne electronic package will be subjected to a high overload of tens of thousands of g for several milliseconds in the chamber during launching,which is easy to cause overload damage.However,the failure analysis of solder joints of projectile-borne electronic package is difficult due to the complex loading environment in the chamber and the coupling effects of various loads.In order to research the failure mechanism of solder joints of projectile-borne electronic package with high overload,the electronic package is tested on an air cannon test platform.The mechanical responses of electronic package under different overload conditions are obtained by through the test,and the damage detection and failure analysis of electronic package are carried out.A numerical simulation model of electronic package solder joints is established and simulated to obtain the mechanical response characteristics of electronic package solder joint under high overload environment.The research results show that the stress of the solder joints in the vertical load direction is less than that in the parallel load direction,and the increase of the load amplitude will increase the solder joint stress,while the increase of the load pulse width will decrease the solder joint stress.It provides a reference for failure analysis of solder joints in projectile-borne electronic packages.

Key words: electronic package solder joint, guided projectile, high overload, numerical simulation, failure mechanism

CLC Number: