بررسی تحلیلی تاثیر مشخصات هندسی پایه مدار الکترونیکی در انتقال ضربه ناشی از جدایش ماهواره

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[11] Ding, J., Zhao, H., Wang, J., Sun, Y., & Chen, Z. (2020). Numerical and experimental investigation on the shock mitigation of satellite-rocket separation. Aerosp Sci Technol, 96, 105538.

[12] Park, H. S., Hwang, D. H., Han, J. H., & Yang, J. (2020). Development of shock-absorbing insert for honeycomb sandwich panel. Aerosp Sci Technol, 104, 105930.

[13] Yan, H., Qin, Z., Chu, F., Zhang, W., Yang, Z., Ming, A., & Wang, X. (2020). Dynamic response of aluminum honeycomb panels to high-frequency laser shock excitations. J Spacecr Rockets, 57(1), 198-201.

[14] Xixiong, W. A. N. G., Tao, Y. U., Huipeng, Y. A. N., Jifeng, D. I. N. G., Zhen, L. I., Zhaoye, Q. I. N., & Fulei, C. H. U. (2021). Application of stress wave theory for pyroshock isolation at spacecraft-rocket interface. Chinese J. Aeronaut., 34(8), 75-86.

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[16] Askari, AR, Lenci, S. Size-dependent response of electrically pre-deformed micro-plates under mechanical shock incorporating the effect of packaging, a frequency-domain analysis, Journal of the Brazilian Society of Int. J. Mech. Sci.. 43 (2021) 1-21.

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