前言决定导弹制导精度与构件可靠性,过去一直是根据飞行数据。最近,考虑到一些经济原因,飞行试验项目受限,以致要求补充一些定性的飞行数据。为此,提出一些实验计划,对获得这些数据的方法进行评定。这些计划中有一个计划已被证明是成功的,这就是让试件承受一个已录制好的模拟飞行环境。助推阶段的冲击和振动数据 The preamble determines missile guidance accuracy and component reliability, which used to be based on flight data. Recently, due to some economic reasons, flight test projects have been limited, requiring some qualitative flight data to be supplemented. To this end, some experimental plans are put forward to evaluate the methods for obtaining these data. One of these plans has proved to be successful, which is to subject the test specimen to a recorded simulated flight environment. Shock and Vibration Data for Boosting Phase