ROCKETS TECHNOLOGY

Numerical Study on Stress and Strain of Heat-preventing Coating of SRM

  • WANG Chunguang ,
  • TIAN Weiping ,
  • CHEN Cong
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  • 1 The 41st Institute of the Fourth Academy, CASC, Xi'an 710025, China
    2 The Fourth Academy, CASC, Xi'an 710025, China
    3 Xi'an Aerospace Chemical Solid Propultion Plant, Xi'an 710025, China

Received date: 2012-08-18

  Online published: 2025-05-26

Abstract

The outside heat-preventing coating of missile (rocket) often cracks, peels off and so on. In order to research the change of stress and strain of outside heat-preventing coating with different temperature, providing a reference for strength analysis, a 3D finite element model was established to study the change characteristics of stress and strain with different temperature. The result shows that the strain of coating will be negative value when the temperature increases, the maximum principal strain criterion should be used to judge whether the material is damaged. The strain of coating will be negative value when the temperature decreases, the Mises stress or maximum principal stress criterion should be used to judge whether the material is damaged.

Cite this article

WANG Chunguang , TIAN Weiping , CHEN Cong . Numerical Study on Stress and Strain of Heat-preventing Coating of SRM[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013 , 33(3) : 98 -101 . DOI: 10.15892/j.cnki.djzdxb.2013.03.016

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