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

摘要

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.