The paper analyzes the influence of various disturbing components arising from a temperature shock of large elastic elements of a small spacecraft structure on the level of microaccelerations of the internal environment. The stability loss of a flat equilibrium shape of an elastic element of a small spacecraft is considered, as well as its all-round expansion when it moves from the shadow area to the illuminated part of the orbit. Conclusions are drawn about the significance of the influence of various factors in modeling the microacceleration field. The results obtained can be used in the design of small technological spacecraft.

中文翻译：

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小型航天器内部环境中温度冲击扰动的各个分量对微加速度水平的影响的意义分析

本文分析了由小型航天器结构的大型弹性元件的温度冲击引起的各种干扰成分对内部环境微加速度水平的影响。考虑了小型航天器的弹性元件的平坦平衡形状的稳定性损失，以及当它从阴影区域移动到轨道的被照亮部分时的全面膨胀。得出了有关在微加速度场建模中各种因素影响的重要性的结论。获得的结果可用于小型技术航天器的设计。