摘要
介绍了固体火箭发动机用D6AC钢喷管壳体的结构及组成。对其加工过程中存在的问题进行了分析,提出了相应的工艺措施,得到了合理的喷管壳体加工工艺方法,顺利实现了工件的批量生产。
In this paper, structure and form of nozzle shell made from D6AC steel applied in solid rocket motor is presented. The existent problem in machining processing is also analyzed. The corresponding technology measures and the suitable methods of machining processing of nozzle shell is obtained, batch production of which is successfully fulfilled.
出处
《航天制造技术》
2014年第1期23-25,29,共4页
Aerospace Manufacturing Technology
