Design and Realization of Recovery System of Chang’e-5 Reentry Spacecraft

IF 0.5 4区 工程技术 Q4 ENGINEERING, AEROSPACE 中国空间科学技术 Pub Date : 2021-01-01 DOI:10.34133/2021/9898756
Wei Huang, W. Rong, Dahai Liu, Changhong Jiang, He Jia, Jinjin Bao, Jishou Fang
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引用次数: 6

Abstract

On December 17, 2020, the Chang’e-5 reentry spacecraft landed safely and brought back the lunar sample without damage. This paper describes the recovery system that has critically contributed to the scientific success of the Chang’e-5 missions and presents the technical requirements and constraints of the recovery system for the Chang’e-5 reentry spacecraft and discusses the design process of the recovery system, including the system composition, working procedure, and some other key aspects. Finally, the ground cover rejection tests and air drop and flight tests were carried out to confirm the design configuration. The results showed that the Chang’e-5 reentry spacecraft recovery system was designed correctly, and its functions and performances met the design requirements. A breakthrough in the recovery technology of the reentry spacecraft was achieved for Chinese first lunar sample-return mission.
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嫦娥五号再入航天器回收系统的设计与实现
2020年12月17日,嫦娥五号再入航天器安全着陆,并毫发无损地带回了月球样本。介绍了对嫦娥五号科学任务成功做出关键贡献的回收系统,提出了嫦娥五号再入航天器回收系统的技术要求和限制条件,并讨论了回收系统的设计过程,包括系统组成、工作流程和其他一些关键方面。最后,进行了地面覆盖物排斥试验、空投和飞行试验,以确定设计构型。结果表明,嫦娥五号再入航天器回收系统设计正确,各项功能和性能满足设计要求。中国首次月球样本返回任务实现了再入航天器回收技术的突破。
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来源期刊
中国空间科学技术
中国空间科学技术 ENGINEERING, AEROSPACE-
CiteScore
1.80
自引率
66.70%
发文量
3141
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