航天器
热的
航空航天工程
保温
电子设备和系统的热管理
机械工程
控制(管理)
材料科学
航天器设计
计算机科学
系统工程
环境科学
工程类
纳米技术
气象学
物理
图层(电子)
人工智能
作者
Robert Consolo,Sandra K. S. Boetcher
出处
期刊:Advances in heat transfer
日期:2023-01-01
卷期号:: 1-50
被引量:8
标识
DOI:10.1016/bs.aiht.2023.04.001
摘要
Spacecraft thermal management is critical for ensuring mission success, as it affects the performance and longevity of onboard systems. A comprehensive overview of the state of the art in spacecraft thermal control solutions, as well as a design methodology framework for efficient and effective thermal management, is provided. Various thermal control solutions, including coatings, insulation, heat pipes, phase-change materials, conductive materials, thermal devices, actively pumped fluid loops, and radiators, are discussed along with the primary sources of heat loading in space. The need for accurate modeling and analysis of the thermal environment to identify appropriate thermal control solutions and design pathways is highlighted. Future innovations in thermal management, such as new materials and technologies that have the potential to further improve the efficiency and effectiveness of thermal control solutions for spacecraft, are explored.
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