DEVELOPMENT AND TEST RESULTS OF CLOSED TWO-PHASE THERMOSYPHONS FOR THE CHINESE MOON EXPLORATION SPACECRAFT CE-3

摘要：

　　This paper will present the development and test results of closed two-phase thermosyphons for the Chinese moon exploration spacecraft, including the lander and the rover.The laboratory models, the prototypes and the engineering models of the loops were designed and tested to satisfy the device thermal control requirements in CE-3.The ground test method how to verify the heat transfer capability of the loops that will operate on the moon surface will be discussed.The thermal vacuum test results of the two phase loop designed for the lunar rover will be presented and discussed

关键词： thermosyphons thermal control moon exploration spacecraft

作者: Hongxing Zhang Jianyin Miao Qing Mo Lu Wang Ziiun Liu Yanchao Xiang

作者单位: Institute of Spacecraft System Engineering China Academy of Space Technology Beijing, P.R.China

会议类型: 国际会议

会议名称: The 11th International Heat Pipe Symposium(第十一届国际热管研讨会)

会议地点: 北京

会议语种:英文

页码: 195-200

在线出版日期: 2013-06-09（万方平台首次上网日期，不代表论文的发表时间）