摘要
文章介绍了采用聚酰亚胺胶带快速抢修生保试验舱温控系统银焊缝渗漏的方法及实施过程中解决的卡箍的不圆度、胶带缠绕的厚度、接头管径的不同等一些关键性技术问题。
The paper introduces tire method to repair quickly leakage of silver welding seams with polyamide tape in the temperature control system of the life-support testing module. Some key technique problems to be solved in practice process are discussed.
出处
《航天器环境工程》
2003年第1期51-55,共5页
Spacecraft Environment Engineering
