关键词: 侵蚀燃烧;复合推进剂;燃烧试验;性能分析;参数分析

Abstract: From the erosive combustion mechanism of solid propellant and combining interrupting burning test of the slab-grain motor with the numerical analysis of the correspondent flow field inside combustion chamber by SIMPLE method,a new method which expresses erosive burning characteristics of solid propellant using the parameters of k2/ε and p on the propellant burning surface was presented. The method was successfully used in the erosive burning study of 4B composite solid propellant,and was comfirmed by experiments.

Key words: Erosive burning;Composite propellant;Combustion test;Performance analysis;Parameter analysis