中国航天器新型热控系统构建进展评述特约

doi:10.7527/S1000-6893.2019.22874

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中国航天器新型热控系统构建进展评述特约

宁献文, 李劲东, 王玉莹, 蒋凡

北京空间飞行器总体设计部空间热控技术北京市重点实验室, 北京 100094

收稿日期:2018-12-26 修回日期:2019-01-10 出版日期:2019-07-15 发布日期:2019-01-24
通讯作者: 李劲东 E-mail:ljd_cast@163.com
基金资助:
国家自然科学基金（11472040）

Review on construction of new spacecraft thermal control system in China

NING Xianwen, LI Jindong, WANG Yuying, JIANG Fan

Beijing Key Laboratory of Space Thermal Control Technology, Beijing Institute of Spacecraft System Engineering(ISSE), Beijing 100094, China

Received:2018-12-26 Revised:2019-01-10 Online:2019-07-15 Published:2019-01-24
Supported by:
National Natural Science Foundation of China (11472040)

摘要/Abstract

摘要： 热控是由工程热物理与航天技术相互促进发展而形成的一门交叉学科，直接影响着航天器的总体设计水平。随着中国航天事业的飞速发展，对热控设计提出了越来越高的要求，并已成为制约中国航天器设计水平的关键瓶颈技术之一。本文综合评述了中国航天器新型热控系统构建的最新研究成果和进展，具体包括：针对载人航天、探月工程等不同任务需求，构建出了相应的新型热控系统，开发出了以泵驱单相流体回路、重力驱动两相流体回路、环路热管与水升华器等为代表的一批新型热控产品。在此基础上，结合中国航天工程实际需求，指出了今后的主要研究方向。

关键词: 航天器, 热控, 热总线, 泵驱流体回路, 环路热管, 水升华器

Abstract: Thermal control is an interdisciplinary subject formed by the mutual promotion of engineering thermophysics and aerospace technology, directly affecting the overall design level of spacecraft. With the rapid development of space industry, thermal control design has appealed to higher requirement that becomes one of the key bottlenecks restricting the level spacecraft design. In this paper, the latest research and progress in the construction of the new thermal control system for spacecraft in China are reviewed. Existing research results show that the new thermal control systems are constructed to meet the needs of different tasks such as manned spaceflight and lunar exploration, developing a number of new thermal products, such as pumped fluid loops, closed two-phase thermosyphons, and loop heat pipe and sublimator. In the end, based on the requirement of the domestic space engineering, this paper outlines the main research directions in thermal control technologies.

Key words: spacecraft, thermal control, thermal bus, pumped fluid loops, loop heat pipe, sublimator

中图分类号:

宁献文, 李劲东, 王玉莹, 蒋凡. 中国航天器新型热控系统构建进展评述特约[J]. 航空学报, 2019, 40(7): 22874-022874.

NING Xianwen, LI Jindong, WANG Yuying, JIANG Fan. Review on construction of new spacecraft thermal control system in China[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(7): 22874-022874.

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中国航天器新型热控系统构建进展评述特约

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