摘要
提出了最小安全飞行高度的有向性问题 .考虑了过载、地形起伏撞地概率和航迹爬升角等因素 ,给出了主要方向上最小安全飞行高度的计算过程 。
The orientation of the minimal safe flight height is researched.The over load,probability of crashing and flight path climbing angle is considered,and the calculation of the minimal safe flight height in main orientations is submitted.
出处
《战术导弹技术》
2003年第2期21-24,29,共5页
Tactical Missile Technology