DocumentCode
518414
Title
Latest research development of spacecraft thermal control technology
Author
Luo, Xiaoling ; Wang, Meijuan
Author_Institution
Qingdao Univ. of Sci. & Technol., Qingdao, China
Volume
5
fYear
2010
fDate
16-18 April 2010
Abstract
With the rapid development of space technology, special thermal design and proper thermal control technologies are essential for ensuring normal spacecraft operation and its instruments. The paper depicts latest research results and application occasion of spacecraft thermal control, especially introduces passive thermal control techniques in detailed, finally proposes current problems need to be solved. Furthermore, it has some reference values to further development of spacecraft thermal control technology.
Keywords
space vehicles; temperature control; normal spacecraft operation; passive thermal control techniques; spacecraft thermal control technology; Design methodology; Equations; Heat transfer; Infrared heating; Solar heating; Space heating; Space technology; Space vehicles; Thermal conductivity; Thermal factors; multilayer insulation; spacecraft; thermal analysis; thermal control;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Engineering and Technology (ICCET), 2010 2nd International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4244-6347-3
Type
conf
DOI
10.1109/ICCET.2010.5486160
Filename
5486160
Link To Document