Design and analysis of a pneumatic test system for shock response spectrum

摘要：

　　Magnitude of the impact test for spacecraft is generally required to be between 1000 g and 2000 g, moreover, the magnitude of some products is more than 3000 g.For high-magnitude impact test of large products, it is difficult for film impact test and drop impact test to meet the test requirements.In order to solve those problems, this paper designed a pneumatic impact test which can perform a high-magnitude impact test, gave the principles of the design and the diagram of the composition of the pneumatic test system, introduced the process and methods of the design of the pneumatic test system, which proposed a theoretical basis for the impact system.

关键词： pneumatic shock response spectrum

作者: Yan Tingfei Xiang Shuhong Shen Zhiqiang ZhangJungan Liu Mo

作者单位: Beijing Institute of Spacecraft Environment Engineering, Beijing, China Beijing Institute of Spacecraft Environment Engineering, Beijing, China;Science and Technology on Re

会议类型: 国际会议

会议名称: the International Conference Vibroengineering-2014

会议地点: 贵阳

会议语种:英文

页码: 46-50

在线出版日期: 2014-11-07（万方平台首次上网日期，不代表论文的发表时间）