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ROCKETS TECHNOLOGY

Influence of Diameter Ratio and Length-diameter Ratio on Structural Integrity of Solid Propellant Grains under Axial Overload

  • LIU Hua ,
  • LI Xuchang
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  • The Missile Institute, Air Force Engineering University, Shaanxi Sanyuan 713800, China

Received date: 2009-05-04

  Online published: 2025-05-28

Abstract

The three-dimensional linear viscoelastic model was used for analyzing the influence of number m and length-diameter ratio on structural integrity of solid propellant grains under axial overload. Nine different numbers m and six length-diameter ratios for fifty four models were selected to measure effect on structural integrity. The results shows that number m and length diameter ratio have cooperative effect on the maximum value of equivalent von Mises stress and strain. If length-diameter is more than 3, it has less influence on the maximum value of equivalent von Mises stress and strain, and it can be referred to the selection of number m and length-diameter in structure design of solid propellant grain.

Cite this article

LIU Hua , LI Xuchang . Influence of Diameter Ratio and Length-diameter Ratio on Structural Integrity of Solid Propellant Grains under Axial Overload[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(2) : 171 -173,267 . DOI: 10.15892/j.cnki.djzdxb.2010.02.048

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Outlines

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