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Journal of Projectiles, Rockets, Missiles and Guidance >

2010 , Vol. 30 >Issue 6: 150 - 151,164

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2010.06.050

ROCKETS TECHNOLOGY

Experiment Research on Ignition Impulsion of Solid Rocket Motor

  • YI Lei ,
  • KOU Junqiang ,
  • LI Weipeng ,
  • DENG Heng ,
  • CHEN Minfang
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  • No. 203 Research Institute of China Ordnance Industries, Xi'an 710065, China

Received date: 2010-07-30

  Online published: 2025-05-28

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Abstract

Under the same conditions of general design of solid rocket motor and propellant design, ignition research under different states and the frequency spectrum analysis were carried out in order to identify the infection factors of impact vibration. The results show that under a same ignition status, ignition pressure will increase by more gunpowder. Similarly, less gunpowder and less granularity of gunpowder are helpful for overloading of the ignition impact vibration.

Key words： solid propellant rocket engine; ignition test; impact vibration; frequency spectrum analysis

Cite this article

YI Lei , KOU Junqiang , LI Weipeng , DENG Heng , CHEN Minfang . Experiment Research on Ignition Impulsion of Solid Rocket Motor[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(6) : 150 -151,164 . DOI: 10.15892/j.cnki.djzdxb.2010.06.050

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