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

被引：8
|
作者：
Huang, Wei [1 ,2 ]
Rong, Wei [1 ,2 ]
Liu, Dahai [1 ,2 ]
Jiang, Changhong [1 ,2 ]
Jia, He [1 ,2 ]
Bao, Jinjin [1 ,2 ]
Fang, Jishou [1 ]
机构：
[1] Beijing Inst Space Mech & Elect, Beijing 100094, Peoples R China
[2] Key Lab Nondestruct Spacecraft Landing Technol CA, Beijing 100094, Peoples R China
来源：
SPACE: SCIENCE & TECHNOLOGY | 2021年 / 2021卷
关键词：
The authors would like to acknowledge the support of the National Medium and Long Term Program for Science and Technology Development of China;
D O I：
10.34133/2021/9898756
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
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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页数：10
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