火箭弹射座椅轨迹发散技术研究  

A Study of Lateral Trajectory Diffusing Techniques for Rocket Ejection Seats

作　　者：马登武[1] 叶文[1] 丁春全 

机构地区：[1]海军航空工程学院军械工程系,山东烟台264001 [2]湖北省襄樊市157信箱,湖北襄樊441003

出　　处：《飞机设计》2006年第2期48-52,共5页Aircraft Design

摘　　要：通过对火箭弹射座椅轨迹发散技术的类型、原理进行分析,建立轨迹发散性能计算模型。经过理论计算和试验验证,侧向轨迹发散火箭技术满足双座弹射救生的要求,有效地解决了FBC-1飞机双座飞行员弹射救生可能发生干扰的问题。On the basis of the analysis of types and principles of trajectory diffusing techniques for rocket ejection seats, the lateral seat trajectory diffusing is modeled. Results of analysis using this technique and data from testing verification show that the lateral trajectory diffusing technique satisfies all requirements for ejection of side-by-side seats and effectively addresses safe escape of the pilots from the FBC-1 twin-seat combat aircraft without interference between the two seats.

关 键 词：火箭弹射座椅 轨迹发散 轨迹干扰 

分 类 号：V412.1[航空宇航科学与技术—航空宇航推进理论与工程]