一种提升导弹舵残骸安全性的主动段程序角设计方法

A Program Angle Design Method of Active Section to Improve the Safety of Missile Rudder Debris

导弹飞行过程中抛落的燃气舵残骸易对行进中的平台或是编队中的其他平台造成威胁。为降低舵残骸的安全风险,本文基于舵残骸对高速行进中平台的安全性需求,提出“先抑后扬”的程序角构型;研究提升导弹舵残骸安全性的弹道设计方法,进行参数优化设计和风险分析。结果表明:该方法有效提升了舵残骸安全性。

The debris of the gas rudder dropped during the missile flight is easy to pose a threat to the moving platform or other platforms in the formation.In order to reduce the safety risk of rudder debris,based on the safety requirements of rudder debris to the high-speed platform,a program angle configuration of"restraining first and then lifting"is proposed.The ballistic design method to improve the safety of missile rudder debris is studied,and the parameter optimization design and risk analysis are carried out.The results show that this method effectively improves the safety of rudder debris.