摘要
阐述了近年来固体火箭发动机装药缺陷失效判定研究的一些进展,目前世界各国还未发现统一而完善的缺陷失效判定方法。根据最近相关领域新技术的出现与军事斗争的需要,展望了这一研究领域未来的发展趋势。
Some progresses of the research on failure criterion for propellant grains with defects in solid rocket motor (SRM) at home and abroad are described. No normalized method of failure criterion has been found in the world. The prospect of developing tendency in this field is stated according to the new progresses of related technologies and the requirement for military field.
出处
《固体火箭技术》
EI
CAS
CSCD
北大核心
2004年第2期126-129,共4页
Journal of Solid Rocket Technology
