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通过理论和实验分析纠正了由于高燃速推进剂允许的ae值较小而造成的高燃速推进剂侵蚀效应大的错觉。指出目前我国广泛应用的ae准则在应用上有一定的局限性。因而对高燃速推进剂的侵蚀准则提出新的建议。
The theoretical and experimental analysis corrects for the illusion that the high burning rate propellant attack erodes due to the low ae allowed by high burning rate propellants. It is pointed out that the ae standard widely used in our country has some limitations in application. Thus putting forward new suggestions on the erosion criteria of high burning rate propellants.