Abstract
The design of thermal control system for a deep space probe is to incorporate advanced active temperature control technology and advanced system design method into the thermal control design of low Earth orbit (LEO) spacecraft fully used for reference, to ensure that the temperature of equipments and structural elements of the deep space probe is within the required range.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References and Related Reading
Xiang Y, Wu Y, Shao X (2007) Investigation on thermal control design methods of deep space spacecraft. Spacecraft Eng 16(6):82–86 (Chinese vision)
Gilmore DG (2002) Spacecraft thermal control handbook—volume I fundamental technologies. The Aerospace Corporation Press, California
Xiang Y, Chen J, Zhang B (2015) Thermal control for jade rabbit rover of Chang’ E-3. J Astronaut 36(10):1203–1209 (Chinese vision)
LyraJC, Novak KS (1997) The mars pathfinder system level solar thermal vacuum test. In: AIAA thermophysics conference, Atlanta
Novak KS, Philips CJ, Sunada ET et al (2005) Mars exploration rover surface mission flight thermal performance. In: The 35th ICES, Rome
Novak KS (2003) Development of a thermal architecture for the mars exploration rovers. Space technology and applications international forum—STAIF, Albuquerque
Bhandari P, Birur G et al (2005) Mars science laboratory thermal control architecture. In: The 35th ICES, Rome
Pantano DR, Dottore F, Tobery W (2005) Utilizing radioisotope power system waste heat for spacecraft thermal management. AIAA, San Francisco
Robson A, Seward E (2005) Thermal design considerations for a mars rover. In: The 35th ICES, Rome
Gardini B, Berner C, Van Casteren J (1999) The technical and programmatic challenge of the international rosetta mission. In: The 50th international astronautical congress, Amsterdam.
Min G, Guo S (1998) Thermal control of spacecraft (Second edition). Science Press, Beijing (Chinese vision)
Hou Z, Hu J (2007) Principles and applications of spacecraft thermal control technology (First edition). China Science and Technology Press, Beijing (Chinese vision)
Xiang Y, Chen J, Zhang B (2014) Thermal balance test of Chang'e-3 “Jade Rabbit” inspector. In: Proceedings of the 2014 annual conference of the Chinese astronautical society, Beijing (Chinese vision)
Vickers JMF, Garipay RR (1968) Thermal design evolution and performance of the surveyor spacecraft. In: AIAA, 5th annual meeting and technical display, Philadelphia
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
Copyright information
© 2021 Beijing Institute of Technology Press and Springer Nature Singapore Pte Ltd.
About this chapter
Cite this chapter
Sun, Z. (2021). Thermal Control Technology. In: Technologies for Deep Space Exploration. Space Science and Technologies. Springer, Singapore. https://doi.org/10.1007/978-981-15-4794-2_9
Download citation
DOI: https://doi.org/10.1007/978-981-15-4794-2_9
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-15-4793-5
Online ISBN: 978-981-15-4794-2
eBook Packages: EngineeringEngineering (R0)