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固体推进剂裂纹扩展研究综述

胡松启 周宴星 刘迎吉 陈静

火箭推进2012,Vol.38Issue(5):86-92,7.
火箭推进2012,Vol.38Issue(5):86-92,7.

固体推进剂裂纹扩展研究综述

Studies on crack extension in solid propellant

胡松启 1周宴星 2刘迎吉 1陈静1

作者信息

  • 1. 西北工业大学,陕西西安710072
  • 2. 中国人民解放军第二炮兵部队,内蒙古自治区呼和浩特010010
  • 折叠

摘要

Abstract

The research status of the crack extension in solid propellant at home and abroad are introduced. Experimental study and theoretical analysis of the crack extension in solid propellant are summarized. The advantages and disadvantages of such study are analyzed. The influences of various factors on crack extension in solid propellant are generalized. The results show that the tension ma- chine and high-speed photography are main means for studying the mechanics characteristic of pro- pellant with crack, and the combustion property of propellant and the extension of crack; the working pressure in combustion chamber, pressure boost rate, style and size of crack, and burning rate of pro- pellant arc the important factors for the crack extension in solid propellant. It is pointed out that it is necessary to research the quantitative relationship between various factors and crack extension.

关键词

固体推进剂/裂纹扩展/增压速率/对流燃烧/断裂韧性

Key words

solid propellant/crack extension/pressure boost rate/convective combustion/fracture toughness

分类

航空航天

引用本文复制引用

胡松启,周宴星,刘迎吉,陈静..固体推进剂裂纹扩展研究综述[J].火箭推进,2012,38(5):86-92,7.

基金项目

总装预研基金项目 ()

火箭推进

OACSTPCD

1672-9374

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