[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]

Journal of Projectiles, Rockets, Missiles and Guidance >

2011 , Vol. 31 >Issue 6: 123 - 125,132

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2011.06.023

ROCKETS TECHNOLOGY

Study of Single Ignition Test of Solid Rocket Motors

  • ZHAO Ruyan ,
  • HUANG Zhiyong ,
  • ZHOU Hongmei ,
  • WANG Bin
Expand
  • Naval Aeronautical and Astronautical University, Shandong Yantai 264001, China

Received date: 2011-03-12

  Online published: 2025-05-30

Fold

Abstract

By Single ignition tests to study the influence of mass of ignition powder on the ignition transient of the igniter and the flow of gas in different mass of ignition powder and the opening pressure of the nozzle closure. The results indicates that the ignition delay of the ignitor decrease with the increase of mass of ignition powder, the ignition delay of motor and the gas-filling time and the pressure in chamber is related with the mass of ignition powder and the opening pressure of the nozzle closure.

Key words： solid rocket motor; ignition; ignition delay

Cite this article

ZHAO Ruyan , HUANG Zhiyong , ZHOU Hongmei , WANG Bin . Study of Single Ignition Test of Solid Rocket Motors[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(6) : 123 -125,132 . DOI: 10.15892/j.cnki.djzdxb.2011.06.023

[an error occurred while processing this directive]

References

[1]
A Ciucci,W A Foster, Jr. R M Jenkins. Results of an experimental investigation of the flow field in the head-end star slot section of a solid rocket motor,AIAA92-3048 [R].1992.
[2]
A Gucci. Flame spreading in the space shuttle head-end star,AIAA 92-3472[R].1992.
[3]
Waesche Rhwoodward,Sargent Williamh，Marchman,J F,et al. Space shuttle solid rocket motor aft-end internal flows[J]. Journal of Propulsion and Power,1989,5(6): 650-656.
[4]
Whitesides R H.Circuferential flow analysis in the aft field joints of the space shuttle solid rocket motor[Z]. 1973.
[5]
Waesche W. Effects of grain slots on flow in a solid rocket motor，AIAA89-2790[R].1989
[6]
韩新波.固体火箭发动机潜入喷管背壁区流动研究[D].西安:西北工业大学,2002.
[7]
王慧,蹇泽群,王华,等.大后翼与主流相互作用的模拟点火试验[J].推进技术,1997,18(3):33-36.
[8]
余贞勇.固体火箭发动机翼槽内火焰传播机理研究[D].西安:西北工业大学,2000.
[9]
Jeffrey D Moore，Kenneth K Kuo，Peter J Ferrara Flame spreading in a simulated fin-slot rocket motor,AIAA-2007-5780[R]. 2007.
[10]
陈汝训.固体火箭发动机设计与研究(下)[M].北京:宇航出版社,1992.
[11]
孙丕忠,秦子增,张晓今,等.微小型固体火箭发动机点火特性试验[J].国防科技大学学报,2000,22(5):23-25.
Options
Outlines

/

〈 〉

[an error occurred while processing this directive]