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 :
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