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刘志强, 赵晨, 曹彦, 陈建岳, 杨敏, 李天义. “嫦娥五号”轨道器供配电系统高比能设计[J]. 深空探测学报(中英文), 2021, 8(3): 237-243. DOI: 10.15982/j.issn.2096-9287.2021.20210007
引用本文: 刘志强, 赵晨, 曹彦, 陈建岳, 杨敏, 李天义. “嫦娥五号”轨道器供配电系统高比能设计[J]. 深空探测学报(中英文), 2021, 8(3): 237-243. DOI: 10.15982/j.issn.2096-9287.2021.20210007
LIU Zhiqiang, ZHAO Chen, CAO Yan, CHEN Jianyue, YANG Min, LI Tianyi. High Specific Energy Design of Power Supply and Distribution System for Chang’E-5 Orbiter[J]. Journal of Deep Space Exploration, 2021, 8(3): 237-243. DOI: 10.15982/j.issn.2096-9287.2021.20210007
Citation: LIU Zhiqiang, ZHAO Chen, CAO Yan, CHEN Jianyue, YANG Min, LI Tianyi. High Specific Energy Design of Power Supply and Distribution System for Chang’E-5 Orbiter[J]. Journal of Deep Space Exploration, 2021, 8(3): 237-243. DOI: 10.15982/j.issn.2096-9287.2021.20210007

“嫦娥五号”轨道器供配电系统高比能设计

High Specific Energy Design of Power Supply and Distribution System for Chang’E-5 Orbiter

  • 摘要: 受制于运载火箭的发射能力,深空探测器对重量指标要求格外苛刻。“嫦娥五号”(Chang’E-5,CE-5)轨道器供配电系统,采用了超高比能的太阳能电池及蓄电池设计、全新的母线拓扑结构,并通过一系列轻量化配电系统设计,将整个飞行器的功率重量比做到国内领先水平。飞行器供配电系统通过地面验证和飞行在轨试验,很好地完成了月面采样返回任务,此技术可为后续深空航天器供配电系统高比能研究和设计提供参考。

     

    Abstract: Limited by the loading capability of launch vehicle, the deep space probe is required to reduce its own weight. Based on the most advanced space power supply technology in China, the power supply and distribution system of Chang’e-5 orbiter adopts ultra-high energy density solar cells and batteries, and invents a new bus topology. Through a series of lightweight power distribution system design, the power to weight ratio of the whole probe reaches the domestic leading level. The power supply and distribution system of spacecraft has passed the ground verification and flight test on in orbit, therefore can be referred for the follow-up research and design of high specific energy of power supply and distribution system of spacecraft.

     

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