摘要
提出一种将尾罩滞留于发射筒内的尾罩分离方案,并对尾罩与弹体的连接方式、尾罩滞留装置方案、燃气排出方式等关键技术问题进行分析,结果表明滞留式尾罩分离方案是可行的。
An arrested trail cover separation project is presented in this paper. The key technology of connection mode between the trail cover and the missile body, arrested trail cover device project and the release form of the high temperature gas are studied. The results shows that the arrested trail cover separation project is available.
出处
《导弹与航天运载技术》
北大核心
2013年第3期12-14,共3页
Missiles and Space Vehicles
关键词
尾罩分离
滞留式
关键技术
Trail cover separation
Arrested form
Key technology
