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The Effect on Small Spacecraft of the Shock Loading Level by Actuation of the Separation System


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Abstract

This paper focuses on the loading of small spacecraft induced by the triggering of separation systems. The article presents the experimental results for the shock loading level of small spacecraft manufactured by Lavochkin Association and analyses the causes of its observed increase. Recommendations are given for changing the testing techniques for the response to shock-impulse loading for similar objects.

About the authors

O. G. Demenko

Lavochkin Association

Author for correspondence.
Email: 3335704@gmail.com
Russian Federation, Khimki, 141400

A. S. Birukov

Lavochkin Association

Email: 3335704@gmail.com
Russian Federation, Khimki, 141400

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