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Journal of Projectiles, Rockets, Missiles and Guidance >

2013 , Vol. 33 >Issue 2: 137 - 140

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2013.02.047

CORRELATION TECHNOLOGY

Simulation and Analysis of Influence Factors of Fairing Separation by ADMAS

  • WANG Bozhe ,
  • WU Jingfeng ,
  • SANG Xijun ,
  • CHEN Wei
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  • The 9th Ouerall Design Department, CASIC, Wuhan 430040, China

Received date: 2012-07-09

  Online published: 2025-05-26

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Abstract

In view of reliability of fairing separation, through the analysis of the separation spring for missile fairing, separation process carried out under the three categories of influencing factors that unlock is not synchronized, the bias of spring stiffness, spring failure fairing, the dynamics simulation was done by Admas, and simulation results were analyzed, the conclusions provide a reference to improve the dynamic performance of missile fairing separation.

Key words： fairing; dynamics simulation; Adams software

Cite this article

WANG Bozhe , WU Jingfeng , SANG Xijun , CHEN Wei . Simulation and Analysis of Influence Factors of Fairing Separation by ADMAS[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013 , 33(2) : 137 -140 . DOI: 10.15892/j.cnki.djzdxb.2013.02.047

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