Articles | Volume 10, issue 1
https://doi.org/10.5194/ms-10-71-2019
© Author(s) 2019. This work is distributed under
the Creative Commons Attribution 4.0 License.
the Creative Commons Attribution 4.0 License.
https://doi.org/10.5194/ms-10-71-2019
© Author(s) 2019. This work is distributed under
the Creative Commons Attribution 4.0 License.
the Creative Commons Attribution 4.0 License.
Design and dynamic analysis of metal rubber isolators between satellite and carrier rocket system
Xibin Cao
CORRESPONDING AUTHOR
School of Astronautics, Harbin Institute of Technology, Harbin,
150001, China
Cheng Wei
School of Astronautics, Harbin Institute of Technology, Harbin,
150001, China
Jiqiu Liang
Fourth Institute of China Aerospace Science and Industry Corporation,
Wuhan, 430000, China
Lixu Wang
School of Astronautics, Harbin Institute of Technology, Harbin,
150001, China
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Latest update: 20 Sep 2026
Short summary
For launching satellite, with the needs of mobility and rapid-responsibility, the vehicle is used for launching. The system inevitably undergoes random vibrations caused by uneven ground excitation, while the camera and other high-precision payloads of the satellite cannot withstand the harsh mechanical environment without isolators. Due to the superior damping properties of MR, this paper designs the simple MR components and provides a feasible design method to absorb vibrations.
For launching satellite, with the needs of mobility and rapid-responsibility, the vehicle is...