Mechanical Shock Wave Suppression Structure in Hold-Down and Release Apparatus of Spacecraft

Author:

Yang Yan1,Liu Wei2,Zhou Hao2,Yang Jianzhong2,Wang Xianping3,Liu Yongquan1

Affiliation:

1. Xi’an Jiaotong University, 710049 Xi’an, People’s Republic of China

2. Beijing Institute of Spacecraft System Engineering, 100094 Beijing, People’s Republic of China

3. Hefei Institute of Physical Science, 230031 Hefei, People’s Republic of China

Abstract

A lightweight and compact structural solution for mechanical shock suppression in spacecraft, such as the hold-down and release apparatus of satellites, is a critical and thorny issue. In this work, a ring-shaped structure is introduced to isolate mechanical waves within cylindrical shells. The underlying mechanism is that the ring-shaped structure undergoes different forms of deformation to counteract different modes of incident waves. A subwavelength Mn-Cu alloy ring is designed as a shock wave barrier in a typical spacecraft hold-down and release apparatus structure with multimodal wave excitation. We experimentally reveal that the Mn-Cu alloy ring reduces the peak value of the acceleration frequency response by 53.4% within a wide frequency range from 1 to 10 kHz. Meanwhile, in the time domain, the instantaneous acceleration peak can be weakened by 37.9%. This work provides a new strategy for shock control of shell structures in aerospace engineering and related fields.

Funder

National Natural Science Foundation of China

National Key Research and Development Program of China

Open Project of National Key Laboratory of Science and Technology on Liquid Rocket Engines

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

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