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Solar System Research

, Volume 52, Issue 7, pp 662–665 | Cite as

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
Article
  • 5 Downloads

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.

Keywords

detonation explosive detonating elongated charge separation mechanism 

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Copyright information

© Pleiades Publishing, Inc. 2018

Authors and Affiliations

  • E. N. Kuzin
    • 1
  • V. I. Zagarskih
    • 1
  • V. V. Efanov
    • 2
  • D. V. Gasheev
    • 1
  1. 1.Military Academy of Strategic Missile ForcesMinistry of DefenseBalashikhaRussia
  2. 2.Lavochkin AssociationKhimkiRussia

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