Design and Realization of Recovery System of Chang’e-5 Reentry Spacecraft
Author(s) -
Huang Wei,
Rong Wei,
Dahai Liu,
Changhong Jiang,
Jia He,
Jinjin Bao,
Jishou Fang
Publication year - 2021
Publication title -
space science and technology
Language(s) - English
Resource type - Journals
ISSN - 2692-7659
DOI - 10.34133/2021/9898756
Subject(s) - reentry , spacecraft , aerospace engineering , spacecraft design , engineering , process (computing) , computer science , systems engineering , operating system , medicine , cardiology
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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