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Spacecraft Thermal Control Technologies


Engels | 20-08-2021 | 376 pagina's

9789811549861

Paperback / softback


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Tekst achterflap

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.

Biografie

Jianyin Miao is an MIT Visiting Professor, Director of the Beijing Key Laboratory of Space Thermal Control Technology and Head Scientist of Heat Pipes at the China Academy of Space Technology. He is also the Academic Leader for space thermal control technology at the China Aerospace Science and Technology Corporation, and a member of the editorial committee of Spacecraft Engineering. Dr. Miao has carried out innovative work on spacecraft thermal control and made outstanding contributions to the success of China's Chang'e-3 lunar missions.   

Qi Zhong is a Research Fellow and an expert on aerospace thermal control at the Institute of Spacecraft System Engineering, CAST. He is also an Academic and Technological Leader at the China Aerospace Science and Technology Corporation. Actively engaged in spacecraft thermal control subsystem design, thermal analysis research and thermal control subsystem development, he has received 6 awards for scientific and technological achievements, holds 20 invention patents and has published more than 40 papers. 

Dr. Qiwei Zhao is a Professor of Space Thermophysics at Institute of Spacecraft System Engineering¿CAST and a member of the editorial committee of Spacecraft Engineering. Dr. Zhao was responsible for the thermal control design and testing of Chinese tracking and data relay satellites. He has also been an advisor on thermal control design for the development of various communication satellite platforms, e.g. the DFH-4S, DFH-4E and DFH-5. 

Professor Xin Zhao serves on the professional committee of the Science and Technology Commission of Institute of Spacecraft System Engineering. He has been actively engaged in research on technologies for thermal control design and thermal analysis. For the past few decades, he has served as the Chief Designer of thermal control subsystems for many spacecraft. He has received several national or ministerial science and technology awards including the Second Class Prize of the National Science and Technology Progress Award.

Kenmerk

Addresses the design and validation of thermal control systems for various types of Chinese spacecraft

Introduces readers to methodologies for implementing thermal control systems in spacecraft, including thermal environments, system design, thermal analysis, and simulation and thermal testing

Includes new advanced thermal control technologies developed in recent years, and their applications

Inhoudsopgave

Introduction.- Space Environment.- Design of Spacecraft Thermal Control Subsystem.- Typical Thermal Control Technologies for Spacecraft.- Typical Thermal Control Design Cases of Spacecraft.- Thermal Analysis Technology.- Spacecraft Thermal Testing.

Details

EAN :9789811549861
Auteur: 
Uitgever :Springer Nature Singapore-Springer Singapore
Publicatie datum :  20-08-2021
Uitvoering :Paperback / softback
Taal :Engels
Hoogte :235 mm
Breedte :155 mm
Dikte :21 mm
Gewicht :569 gr
Status :POD (Beschikbaar als print-on-demand.)
Aantal pagina's :376
Reeks :  Space Science and Technologies
Keywords :  Heat and Mass Transfer; Temperature Uniformity; Thermal Characteristics; Space Thermal Environment; Spacecraft Thermal Control System; Spacecraft Thermal Control Design; Thermal Control Technology; Heat Acquisition; Heat Transportation; Energy Storage; Heat Insulation; temperature measurement; Thermal Design Example; Thermal Simulation and Analysis; thermal testing; Pumped Fluid Loop; Phase-Change Material