Features of Testing the Impact Strength of the Landing Module of the Exomars-2020 Interplanetary Vehicle


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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.

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O. Demenko

Lavochkin Association

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Email: 3335704@gmail.com
俄罗斯联邦, Khimki, Moscow oblast, 141402

A. Biryukov

Lavochkin Association

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Email: birukov@laspace.ru
俄罗斯联邦, Khimki, Moscow oblast, 141402

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