“…The former is that, from a microscopic viewpoint, temperature differential fusion creates the thermal cycle effect, electromagnetic wave impact, and other elements that lead to vacancies in the material's lattice and result in the embrittlement failure of the structure. Second, from the macro viewpoint, the spacecraft's exposure to space debris and other floating objects, as well as fatigue damage brought on by the vibration of the spacecraft during the mission cycle, present a significant challenge for the spacecraft's long lifespan, high reliability, and high-quality performance [4] . Currently, when designing spacecraft and other platforms, engineers must take into account not only the platforms' own structures and functions but also the influence that rising launch loads will have on the mechanical environment.…”