反坦克火箭后喷危险界解决方法研究  

A Study on Back-Ejection's Danger Boundary of Anti-Tank Rocket

作　　者：马宏伟[1] 

机构地区：[1]南京理工大学动力工程学院,江苏南京210094

出　　处：《弹箭与制导学报》2004年第S5期164-165,168,共3页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：反坦克火箭武器后喷危险界随着火箭的推力增大而增大,后喷危险界的增大给性能优良的武器带来使用上的限制。文中对后喷危险界产生的原因和减小危险界的方法进行了理论和实验方面的研究。指出了减小后喷危险界的可行途径。With rocket's propulsion force increase,back-ejection's danger boundary is enlarged.Weapon which is good in performance can be limited in use because of the danger boundary's enlargement.The causes of danger boundary are researched through theory and experiments in this article.Finally approaches to diminish the danger boundary are put forward.

关 键 词：火箭 后喷危险界 后抛物 易损性 

分 类 号：E927[军事—军事装备学]