[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 >

2013 , Vol. 33 >Issue 1: 132 - 134

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2013.01.001

ROCKETS TECHNOLOGY

The Study on Antiablative Property of C /C Composites

  • WANG Dewen ,
  • YANG Yuecheng ,
  • ZHA Bailin ,
  • HE Xiaopeng
Expand
  • The Second Artillery Engineering University，Xi’an 710025，China

Received date: 2012-05-05

  Online published: 2025-05-24

Fold

Abstract

According to environment of solid rocket，C/C composites are ablated in a flame，which is produced by oxygen and aviation kero sene． In order to simulate solid rocket motor，some Al2O3 particles were appended in the flame． Through calculating the temperature field and velocity field of the HVOF，the parabola distribution of the HVOF was found． Through calculating the ablation ratios，scanning the ab lation area，and combining the flame characters，the ablating mechanisms of C/C composites were found．

Key words： carbon-carbon composites; Al2O3 particle; ablation /erosion; high velocity oxygen fuel

Cite this article

WANG Dewen , YANG Yuecheng , ZHA Bailin , HE Xiaopeng . The Study on Antiablative Property of C /C Composites[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013 , 33(1) : 132 -134 . DOI: 10.15892/j.cnki.djzdxb.2013.01.001

[an error occurred while processing this directive]

References

[1]
张福祥. 火箭燃气射流动力学[M]. 北京: 国防工业出版社, 2004. 63- 66.
[2]
张贵田. 高压补燃液氧煤油发动机[M]. 北京: 国防工业出版社, 2005: 1- 226.
[3]
L M Manocha, E Fitzer. Carbon Reinforcements and C/CCom-posites[M]. Springer, 1998.
[4]
丘哲明. 固体火箭发动机材料与工艺[M]. 北京: 宇航出版社, 1995.
[5]
刘红林, 金志浩, 郝志彪,等. 化学液相沉积制备的炭/炭复合材料烧蚀性能研究[J]. 固体火箭技术, 2005, 28(1): 57- 59.
Options
Outlines

/

〈 〉

[an error occurred while processing this directive]