摘要
对战术导弹固体火箭发动机的结构可靠性评估方法及其应用作了述评，并以某空空导弹发动机为例进行了计算、比较。与其他方法相比，有验前信息的贝叶斯法能较好地反映发动机的实际结构可靠性水平，是一种较为合理、有效的评估方法。
In this paper,some assessments for structural reliability of tactic missile solid rocket motors and their applications are reviewed. Some calculations and comparisons are made based on the firing test results of some air air missile motor. The more rational, effective assessment is in the engineering development of solid rocket motor and a developing tendency in the future are presented.
出处
《上海航天》
1999年第4期37-41,共5页
Aerospace Shanghai
