The erosive property and principle of copper-infiltrated graphite as solid rocket motor(SRM) throat insert and tailpipe nozzle bushing are presented.

 
  • 介紹了石墨滲銅材料作為固體火箭發(fā)動(dòng)機(SRM)喉襯與長(cháng)尾管襯套的燒蝕特性和機理。
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