可控式折叠翼火箭弹的增程技术探究  

Research on Extended Range Technique for Rocket with Controllable Folded Wing

作　　者：钟世宏[1] 孙巍[1] 乔园园[1] 杨立合[1] 张进[1] 

机构地区：[1]西安长峰机电研究所,西安710065

出　　处：《弹箭与制导学报》2014年第2期94-97,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：文中通过对现有火箭弹增程技术方案的分析,指出其存在的局限性和不足,提出可控式折叠翼技术的火箭弹增程方案,对实施新方案后的相关性能参数作了定性分析,同时给出相应的弹道规划设计,针对可控式折叠弹翼的相关结构设计工作,提出具体的设计思路和注意事项,并介绍了可控式折叠弹翼用地面试验设备的设计方案,为火箭弹性能的进一步完善提供了新的途径。Through analysis on existing extended range technical programs,in this paper,not only their limitations and shortcomings were pointed out,but also a new extended range technical program was raised. The relative property parameters of the new program were analyzed qualitatively. The according trajectory planning and design were also given in this paper. Specific design methods and considerations were put forward for the structural design of the controllable folded wing. The design method was introduced for the ground test equipment of the folded wing rockets. A new way was provided for perfection of the rocket performance.

关 键 词：火箭弹 增程 可控式折叠弹翼 结构设计 地面试验设备 

分 类 号：TJ413.4[兵器科学与技术—火炮、自动武器与弹药工程]