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月球车热管理系统质量优化
引用本文:马林, 刘学超, 冯孝辉, 等. 月球车热管理系统质量优化[J]. 航天器环境工程, 2020, 37(2): 172-178doi:10.12126/see.2020.02.012
作者姓名:马林  刘学超  冯孝辉  吴宏  闻洁  于兆吉
作者单位:1.航天东方红卫星有限公司,北京 100094;2.北京航空航天大学 能源与动力工程学院,航空发动机气动热力重点实验室,北京 100083
摘    要:月球车热管理系统是为了确保车辆在恶劣的月球环境下正常工作的重要系统,质量是其重要的评价指标。通过对热管理系统模型的热网络分析,文章对影响月球车热管理系统质量的几个重要因素,如辐射器出口温度、热回路管径、冷媒流量、电控制元件、管路设计和阀门应用等分别进行计算,分析了这些因素对系统质量的影响规律;在此基础上,根据探月车辆模型环境参数和工作参数,利用搜索寻优法确定了使系统质量最小的最佳系统结构参数和操作参数,实现了热管理系统的初步质量优化分析。研究结果对于工程应用具有一定的参考意义。

关 键 词:热管理系统   热控制   月球车   质量优化
收稿时间:2019-07-22
修稿时间:2020-03-30

Mass optimization of thermal management system for lunar rover
MA L, LIU X C, FENG X H, et al. Mass optimization of thermal management system for lunar rover[J]. Spacecraft Environment Engineering, 2020, 37(2): 172-178doi:10.12126/see.2020.02.012
Authors:MA Lin  LIU Xuechao  FENG Xiaohui  WU Hong  WEN Jie  YU Zhaoji
Affiliation:1. DFH Satellite Co. Ltd., Beijing 100094, China;2. National Key Laboratory on Aero-engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
Abstract:The function of thermal management system for lunar rover is to ensure the temperature in an appropriate range, and, at the same time, within a mass constraint. By analyzing the thermal network of the system, several essential factors affecting the system weight are computed, such as the exit temperature of the radiator, the tube diameter of the thermal loop, the mass of the cooling-fluid, as well as the electronic control components, the tube design and the valve usages, to determine their influencing laws to the system weight. Based on that, the searching for the optimal structural and operation parameters of the rover system is implemented according to the environment parameters and working parameters of the lunar rover model. The optimized parameters are obtained for light weight purpose. Thus the principal analysis of mass optimization of the thermal management system are realized, with some reference value for engineering applications.
Keywords:thermal management system  thermal control  lunar rover  mass optimization
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