Engineering Methodology for Assessment оf Spacecraft Structure Shock Load Levels During Pyromechanical Separation

E. N. Kuzin; V. I. Zagarskih; V. V. Efanov; D. V. Gasheev

doi:10.1134/S0038094618070146

Engineering Methodology for Assessment оf Spacecraft Structure Shock Load Levels During Pyromechanical Separation

作者: Kuzin E.N.¹, Zagarskih V.I.¹, Efanov V.V.², Gasheev D.V.¹
隶属关系:
1. Military Academy of Strategic Missile Forces
2. Lavochkin Association
期: 卷 52, 编号 7 (2018)
页面: 662-665
栏目: Article
URL: https://journals.rcsi.science/0038-0946/article/view/171205
DOI: https://doi.org/10.1134/S0038094618070146
ID: 171205

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详细

In this paper, we consider an algorithm for estimating the dynamic shock loads on sensitive units, assemblies, systems, and payloads of a spacecraft, as well as on precision elements of its construction occurring near separation belts that are based on linear cumulative and noncumulative pyromechanisms.