中国月球探测有效载荷热控技术研究进展OA
Advances in Thermal Control Technology for Chinese Lunar Exploration Payloads
有效载荷热控是保障月球探测科学仪器可靠运行、实现科学数据精准获取的关键技术.本文结合中国月球探测工程的实施进展,基于载荷科学目标、工程应用特征与热控任务特点,梳理了月球有效载荷热控系统的设计流程;根据有效载荷与平台热控的耦合关系,将有效载荷热控技术体系划分为3大类别,系统地总结了各类别的研究成果与发展情况.面向后续月球科研站建设、长期月面探测及多载荷协同探测等任务需求,明确了中国月球探测有效载荷热控技术的后续重点研究方向.
Payload thermal control is a critical technology for the reliable operation of scientific instruments in lunar exploration and for the accurate acquisition of scientific data.This paper reviews the design process of thermal control systems for lunar payloads,considering the implementation progress of China's lunar exploration engineering,as well as the payload's scientific objectives,engineering application characteristics,and thermal control task features.Based on the coupling relationship between payload thermal control and platform thermal control,the technical system for lunar payload thermal control is categorized into three major areas,with a systematic summary of the research achievements and development status of each branch.To address the requirements of future missions,including lunar research station construction,long-term lunar surface exploration,and coordinated multi-payload exploration,this paper identifies key directions for future research on thermal control technology for China's lunar exploration payloads.
张亚男;宁献文;王雷;薛长斌;徐海涛;耿浩
中国科学院国家空间科学中心,北京 100190||哈尔滨工业大学机电工程学院,哈尔滨 150001北京空间飞行器总体设计部航天器热控全国重点实验室,北京 100094中国科学院国家空间科学中心,北京 100190中国科学院国家空间科学中心,北京 100190中国科学院国家空间科学中心,北京 100190中国科学院国家空间科学中心,北京 100190
航空航天
月球探测有效载荷热控热设计热开关
lunar explorationlunar payloadthermal controlthermal designthermal switch
《南京航空航天大学学报(自然科学版)》 2026 (4)
709-719,11
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