航空兵器Issue(2)：50-52,60,4.
某发动机壳体烧穿故障分析及改进设计
Burned-Through Failure Analysis of Solid Rocket Motor Case and Improved Design
邢志浩 1王虎干 1房雷2
作者信息
- 1. 中国空空导弹研究院，河南洛阳 471009
- 2. 航空制导武器航空科技重点实验室，河南洛阳 471009
- 折叠
摘要
Abstract
The factors resulting in solid rocket case burned-through are analyzed by FTA method, and validited by flow simulation and the ground simulation overload test .According to the analysis result, the improved design and test are carried out .The result shows that the improved design is effective , which will guarantee the solid rocket motor safe and reliable under practical working .关键词
固体火箭发动机/烧穿/故障分析/改进设计/仿真Key words
solid rocket motor/burned-through/failure analysis/improved design/simulation分类
航空航天引用本文复制引用
邢志浩,王虎干,房雷..某发动机壳体烧穿故障分析及改进设计[J].航空兵器,2013,(2):50-52,60,4.
