Based on pressure and high low temperature cycling tests and theoretic analysis, the threaded joint parts filled with sealing glue compound show excellent seal ability, and can be applied to SRM.
通过压力、高低温循环等大量的试验和理论分析表明：采用填充密封胶的螺纹联接密封结构具有优异的密封性，适宜在固体火箭发动机环境中应用。
A new seal structure suited to solid rocket motors (SRM) is introduced, and threaded joint structures and sealing glue compound are studied.
提出了一种适用于固体火箭发动机(SRM)的新型密封结构，并对应用于特定尺寸的螺纹联接结构方式、胶种选择进行了研究。
A new seal structure suited to solid rocket motors (SRM) is introduced, and threaded joint structures and sealing glue compound are studied.
提出了一种适用于固体火箭发动机(SRM)的新型密封结构，并对应用于特定尺寸的螺纹联接结构方式、胶种选择进行了研究。
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