中国机械工程2009，Vol.20Issue(22)：2766-2771,6.
航天器元件多参数综合可靠性环境试验研究综述
Research Summary of the Multiparameter Combined Environmental Test of Spacecraft Component Reliability
摘要
Abstract
The background, significance and recent research situation at home and abroad were summarized herein. The reseach procedure and technology scheme of the high accelaration, vibration, temperature, air pressure and noise combined environmental test model machine was preferred. Some key technologies such as the dynamic banance of the centrifuge, the redress system of motion parts of the vibration table, the vibration--control of the arm of the centrifuge, the temperature field control and the sound field control in centrifugal field were analyzed and the corresponding solutions were put forward.关键词
航天器元件/多参数/综合环境试验/可靠性/关键技术Key words
spacecraft component/ multiparameter/ combined environmental test/ reliability/ key technology分类
航空航天引用本文复制引用
方兵,沈润杰,何闻,郭吉丰,贾叔仕..航天器元件多参数综合可靠性环境试验研究综述[J].中国机械工程,2009,20(22):2766-2771,6.基金项目
国家863高技术研究发展计划资助项目(2007AA042440) （2007AA042440）
