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本文的目的是把《航天飞机组装构型垂直地面振动试验报告》作一摘要。打算先用一些统计数据来说明一下这个试验的规模大小,然后再讲航天飞机组装构型垂直地面振动试验本身的情况、试验的目的、试验与分析的相关性,以及由于试验分析相关性问题而进行的实时研究。然后讨论目前大型试验中存在的问题以及今后可能采取的解决办法。飞行器专用的试验时间为10个月,这就是说,所有有关的基本组件都是大约使用这么长
The purpose of this paper is to give an abstract of the “Report on Vertical Ground Vibration Test of Spacecraft Assembly Structure”. Intend to use some statistical data to illustrate the size of the test, and then talk about the spacecraft assembly configuration vertical ground vibration test itself, the purpose of the test, the correlation between the test and analysis, and due to the experimental analysis of the correlation and Real-time research conducted. Then we discuss the problems that exist in the current large-scale trials and the possible solutions to be adopted in the future. The aircraft-specific test time is 10 months, which means that all the relevant basic components are used about this long