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.
出处
《飞机设计》
2006年第2期48-52,共5页
Aircraft Design
关键词
火箭弹射座椅
轨迹发散
轨迹干扰
rocket ejection seat
track diffusing
track interference
