一种火箭弹头体分离系统研究  

Research of A Stage Separation System for Rocket Projectile

作　　者：李小笠[1] 陶江源[1] 唐平[1] 吴玉均 杨晓成 

机构地区：[1]中国工程物理研究院结构力学研究所,四川绵阳621900 [2]西安庆华电器集团有限公司,陕西西安710025

出　　处：《火工品》2009年第5期1-4,共4页Initiators & Pyrotechnics

摘　　要：根据火箭弹对头体分离系统的要求,结合火箭弹的结构特点,提出了活塞式燃气分离方案,设计了分离形式和电缆线断线方法,并进行了分离系统的性能试验。试验结果表明:该分离系统工作可靠,分离形式和电缆线断线的设计合理,抛射组件未出现明显变形。通过试验,还获得了相对分离速度和火药药量的关系。该分离系统可用于弹径较小、壳体壁厚较薄,且相对分离速度要求较高的火箭弹进行头体分离。Aiming at stage separation requirement of rocket projectile as well as the characteristic of rocket, the piston-type separation device was presented. The separation form and cable-cut technique were researched, and the performance of the piston-type separator was tested. The results showed that the rocket projectile could be separated completely, the separation form and the cable-cut design were effective and the projected component had no evident deformation. The relationship of relative separation velocity and the mass of powder was obtained. The separation system can be used for the separation of rocket projectile with small calibre, thin shell and high relative separation velocity.

关 键 词：分离装置 火箭弹 头体分离 活塞 相对分离速度 

分 类 号：TJ459[兵器科学与技术—火炮、自动武器与弹药工程]