Theoretical and experimental study of a method for the protection of spacecraft from high–speed particles
- Авторы: Gerasimov A.V.1, Dobritsa D.B.2, Pashkov S.V.1, Khristenko Y.F.1
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Учреждения:
- Tomsk State University
- Lavochkin Research and Production Association
- Выпуск: Том 54, № 2 (2016)
- Страницы: 118-126
- Раздел: Article
- URL: https://journals.rcsi.science/0010-9525/article/view/153322
- DOI: https://doi.org/10.1134/S0010952516020015
- ID: 153322
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Аннотация
In this paper, we perform numerical simulation and experimental determination of the limiting resistance of the spacecraft design elements used when developing anti-meteorite protection of spacecraft as well as protection against space debris. One possible way to increase the efficiency of protective shields and satisfy the requirements of the mass characteristics of the latter is the use of mesh barriers.
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Об авторах
A. Gerasimov
Tomsk State University
Автор, ответственный за переписку.
Email: ger@mail.tomsknet.ru
Россия, Tomsk, 634050
D. Dobritsa
Lavochkin Research and Production Association
Email: ger@mail.tomsknet.ru
Россия, Khimki, Moscow oblast, 141400
S. Pashkov
Tomsk State University
Email: ger@mail.tomsknet.ru
Россия, Tomsk, 634050
Yu. Khristenko
Tomsk State University
Email: ger@mail.tomsknet.ru
Россия, Tomsk, 634050
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