This book presents fundamental theories, design and testing
methodologies, and engineering applications concerning spacecraft
thermal control systems, helping readers gain a comprehensive
understanding of spacecraft thermal control systems and technologies.
With abundant design methods, advanced technologies and typical
applications to help them grasp the basic concepts and principles of
engineering applications, it is mainly intended for engineering and
technical staff engaged in spacecraft thermal control areas.
The book discusses the thermal environments commonly used for space
flight missions, rules and regulations for system design, thermal
analysis and simulation, and thermal testing methods, as well as the
design and validation of the thermal control systems for Chinese
spacecraft, such as the Shenzhou spacecraft and Chang'e Lunar Lander and
Rover. It also introduces them to communication and remote sensing
satellites and presents advanced thermal control technologies developed
in recent years, including heat transfer, heat insulation, heating,
refrigeration and thermal sensor technologies.
Addressing the design and validation of thermal control systems for
various types of Chinese spacecraft, the book offers a valuable
theoretical and practical reference guide for researchers and engineers
alike.