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A compact payload system for two formation-flying micro-satellites in the Chang'e IV mission
Zhou, Li; An, Junshe; Wang, Zhugang; Wu, Lin; Zhao, Fei; Zhang, Jinxiu; Kong, Xianren
Department空间技术部
Source Publication2018 IEEE AEROSPACE CONFERENCE
2018
ISSN1095-323X
ISBN978-1-5386-2014-4
AbstractTwo micro satellites will be manufactured and launched to the farside of the Moon by piggybacking on the CHANG'E-4 mission to make astronomical super-long wavelength observation, taking the advantage of the excellent electromagnetic environment on the Moon-farside. This paper proposes a highly compact payload system for this purpose, regarding the extreme conditions of limited mass, volume, power and cost. The functional units of the proposed payload system and related key technologies are described in detail. Experimental results verify the functional performance of our design. This project will be part of Chinese first star-star interferometry astronomical observation.
Conference NameIEEE Aerospace Conference
Conference DateMAR 03-10, 2018
Conference PlaceBig Sky, MT
Indexed ByCPCI
Document Type会议论文
Identifierhttp://ir.nssc.ac.cn/handle/122/7082
Collection空间技术部
Recommended Citation
GB/T 7714
Zhou, Li,An, Junshe,Wang, Zhugang,et al. A compact payload system for two formation-flying micro-satellites in the Chang'e IV mission[C],2018.
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