Engineering Methodology for Assessment оf Spacecraft Structure Shock Load Levels During Pyromechanical Separation
- Авторы: Kuzin E.N.1, Zagarskih V.I.1, Efanov V.V.2, Gasheev D.V.1
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Учреждения:
- Military Academy of Strategic Missile Forces
- Lavochkin Association
- Выпуск: Том 52, № 7 (2018)
- Страницы: 662-665
- Раздел: Article
- URL: https://journal-vniispk.ru/0038-0946/article/view/171205
- DOI: https://doi.org/10.1134/S0038094618070146
- ID: 171205
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Аннотация
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.
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Об авторах
E. Kuzin
Military Academy of Strategic Missile Forces
Автор, ответственный за переписку.
Email: arvsn@mil.ru
Россия, Balashikha, 143900
V. Zagarskih
Military Academy of Strategic Missile Forces
Email: arvsn@mil.ru
Россия, Balashikha, 143900
V. Efanov
Lavochkin Association
Email: arvsn@mil.ru
Россия, Khimki, 141402
D. Gasheev
Military Academy of Strategic Missile Forces
Email: arvsn@mil.ru
Россия, Balashikha, 143900
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