Email this article Engineering Methodology for Assessment оf Spacecraft Structure Shock Load Levels During Pyromechanical Separation
- Authors: Kuzin E.N.1, Zagarskih V.I.1, Efanov V.V.2, Gasheev D.V.1
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Affiliations:
- Military Academy of Strategic Missile Forces
- Lavochkin Association
- Issue: Vol 52, No 7 (2018)
- Pages: 662-665
- Section: Article
- URL: https://journal-vniispk.ru/0038-0946/article/view/171205
- DOI: https://doi.org/10.1134/S0038094618070146
- ID: 171205
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Abstract
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.
About the authors
E. N. Kuzin
Military Academy of Strategic Missile Forces
Author for correspondence.
Email: arvsn@mil.ru
Russian Federation, Balashikha, 143900
V. I. Zagarskih
Military Academy of Strategic Missile Forces
Email: arvsn@mil.ru
Russian Federation, Balashikha, 143900
V. V. Efanov
Lavochkin Association
Email: arvsn@mil.ru
Russian Federation, Khimki, 141402
D. V. Gasheev
Military Academy of Strategic Missile Forces
Email: arvsn@mil.ru
Russian Federation, Balashikha, 143900
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