1. Lunar Exploration and Space Engineering Center,Beijing 100190,China; 2. Beijing Insititute of Spacecraft System Engineering,Beijing 100094,China; 3. Shanghai Academy of Spaceflight Technology,Shanghai 201109,China; 4. Beijing Institute of Tracking and Telecommunications Technology,Beijing 100094,China; 5. China Academy of Launch Vehicle Technology,Beijing 100076,China
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Received
Published Online
2021-06-20
2021-06-20
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Abstract
In response to the requirements of lunar sampling and return mission, based on the development of our country’s launch vehicle and the technical foundation in the first and second phases of the lunar exploration project, a multi-planned and multi-round iterative trade-off analysis has been made on the overall plan of the detector, the composition of the functional modules, the launch method, the flight process, etc., and the module composition, main flight process and “Chang’E-5” engineering design process of “Chang’E-5” detector have been gradually optimized and determined. The result fully proves that the scheme is in line with our country’s lunar exploration project development plan and aerospace technology development expectations, and thus is advanced and feasible. The NAFVO trade-off design method adopted in the design process can provide a useful reference for the design of complex and large-scale aerospace engineering schemes.
PEI Zhaoyu, REN Junjie, PENG Jing, WANG Qiong, HU Zhenyu, LI Haitao, HUANG Lei, GENG Guangyou.
Overall Scheme Trade-off Design of Chang’E-5 Mission.
Journal of Deep Space Exploration, 2021, 8(3): 215-226 DOI:10.15982/j.issn.2096-9287.2021.20210028