Email this article Features of Testing the Impact Strength of the Landing Module of the Exomars-2020 Interplanetary Vehicle
- Authors: Demenko O.G.1, Biryukov A.S.1
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Affiliations:
- Lavochkin Association
- Issue: Vol 53, No 7 (2019)
- Pages: 624-630
- Section: Article
- URL: https://journals.rcsi.science/0038-0946/article/view/171569
- DOI: https://doi.org/10.1134/S0038094619070037
- ID: 171569
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Abstract
In this paper, we analyze the problems of testing the impact strength of the Exomars-2020 spacecraft on landing. The design features of the landing module of the Exomars-2020 spacecraft are considered as the object of impact tests. Here, we discuss the main solutions implemented while ensuring the impact strength of the Exomars-2020 spacecraft. Recommendations on the development of the impact testing system for prospective spacecraft are provided.
About the authors
O. G. Demenko
Lavochkin Association
Author for correspondence.
Email: 3335704@gmail.com
Russian Federation, Khimki, Moscow oblast, 141402
A. S. Biryukov
Lavochkin Association
Author for correspondence.
Email: birukov@laspace.ru
Russian Federation, Khimki, Moscow oblast, 141402
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