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Modeling the micro-acceleration field in the protected zone of vibration-proof devices for implementation of gravity-sensitive processes on board a small technological spacecraft

https://doi.org/10.25206/2588-0373-2023-7-2-65-72

Abstract

In this paper, models of the micro-acceleration field in the protected zone of various vibration-proof devices are constructed. An automatic rotary platform and a vibration-proof device based on the magnetic principle of operation are considered. Numerical simulation has been carried out for the platform of a small spacecraft of the Aist-2 type. Conclusions are drawn about the possibility of using vibration-proof devices when conducting gravity-sensitive processes on board a technological ICA. The results obtained can be used in the analysis of the satisfaction of conditions for micro-accelerations.

About the Authors

A. V. Sedelnikov
Samara National Research University
Russian Federation

Sedelnikov Andrey Valeryevich - Doctor of Technical Sciences, Professor, Professor of Space Engineering Department, SPIN-code: 3987-6997. AuthorID (SCOPUS): 23013232300. ResearcherID: G-4444-2017.

Samara, Moskovskoye sh., 34, 443086



A. S. Taneeva
Samara National Research University
Russian Federation

Taneeva Anastasiya Sergeevna - Graduate Student of Space Engineering Department, Engineer of NII-219 (Research Institute of Space Engineering), Engineer and Assistant of Space Engineering Department, SPIN-code: 8816-1930. AuthorID (SCOPUS): 57205365815.

Samara, Moskovskoye sh., 34, 443086



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For citations:


Sedelnikov A.V., Taneeva A.S. Modeling the micro-acceleration field in the protected zone of vibration-proof devices for implementation of gravity-sensitive processes on board a small technological spacecraft. Omsk Scientific Bulletin. Series Aviation-Rocket and Power Engineering. 2023;7(2):65-72. (In Russ.) https://doi.org/10.25206/2588-0373-2023-7-2-65-72

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