ROCKETS TECHNOLOGY

Study on Grains of Regressive Burning Law Selection Criteria

  • ZHAN Junbiao ,
  • XIANG Shenghai ,
  • LI Shipeng ,
  • WANG Limin ,
  • YU Chao ,
  • WANG Di
Expand
  • 1 School of Equipment Engineering, Shenyang Ligong University, Shenyang 110159, China
    2 Jinxi Industries Group Co. Ltd, Taiyuan 030027, China
    3 School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
    4 Jilin Jiangji Company, Northeast Industries Group Co. Ltd, Jilin Jilin 132021, China

Received date: 2014-10-12

  Online published: 2025-05-28

Abstract

Based on geometrical law of burning, the discipline of burning area changing with burned web thickness for variety of grain types was deduced. The regressive burning of star-shaped grain, wheel-shaped grain, sleeve-shaped grain and short tubular grain was analyzed. Results show that the regressive buring of star-shaped grain and wheel-shaped grain are larger, and the adjustable range of the degression buring is large. Regressive burning of sleeve-shaped grain and short tubular grain is smaller. When the degressive nature is small, the short tubular grain is selected preferentially. When the star angle of the star-shaped grain and the wheel arm of the wheel-shaped grain have the same number, further more, they have the same regressive burning; the filling factor and web thickness of star-shaped grain will be larger than wheel-shaped grain. When degressive nature is large, star-shaped grain is selected preferentially.

Cite this article

ZHAN Junbiao , XIANG Shenghai , LI Shipeng , WANG Limin , YU Chao , WANG Di . Study on Grains of Regressive Burning Law Selection Criteria[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(5) : 85 -91 . DOI: 10.15892/j.cnki.djzdxb.2015.05.022

References

[1]
杨月诚. 火箭发动机理论基础[M]. 西安: 西北工业大学出版社, 2010.
[2]
Hawkins David K, Campbell Carol J. Advanced designs for high pressure, high performance solid propellant rocket motor: US 6682615[P]. 2004.
[3]
Roy J Hartf ield, John E Burkhalter, Rhonald M Jenkins. Analytical development of a slotted grain solid rocket Motor[C] // 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Indianapolis: AIAA, 2002: 2002-4298.
[4]
覃光明, 卜昭献, 张晓宏. 固体推进剂装药设计[M]. 北京: 国防工业出版社, 2013.
[5]
王元有. 固体火箭发动机设计[M]. 北京: 国防工业出版社, 1984.
[6]
王春利, 孙维申, 邹广宝. 开槽管型装药(减面形)的设计与应用研究[J]. 固体火箭技术, 1996, 19 (3): 41-45.
[7]
张为华. 星孔药柱设计研究[J]. 推进技术, 1993 (1): 51-56.
[8]
陈步学, 王凌燕, 吴心平. 星孔装药燃面退移图形显示研究[J]. 推进技术, 1996, 17 (6): 33-38.
[9]
秦飞. 固体火箭发动机复杂装药燃面算法研究[D]. 西安: 西北工业大学, 2003.
[10]
Herman R D, Butler JH. Subsystems for the extended range interceptor (ERINT-4) missile, AIAA 92-3872[R]. 1992.
[11]
LTC Patrick Oreilly, Ed Walters. The patriot PAC-3 missile program an affordable integration approach, AD-A 319 957[R].
[12]
魏志军, 张平, 方蜀州. 美国“爱国者 PAC-3”型导弹主发动机装药药型反设计[J]. 固体火箭技术, 2004, 27 (2): 114-116.
Outlines

/