DocumentCode
1715600
Title
Calculating radiation force on carbon fiber gossamer space sailcraft
Author
Whites, K.W. ; Knowles, T.R.
Author_Institution
Dept. of Electr. Eng., Kentucky Univ., Lexington, KY, USA
Volume
3
fYear
2001
Firstpage
326
Abstract
Solar sails are ultra-lightweight, propellantless spacecraft that obtain propulsion from the Sun\´s electromagnetic emissions or other concentrated sources such as powerful lasers. Advances in materials processing and deployment practices have led to the development of practical missions for such sails. In order for sailcraft to meet the requirements of future missions, sail materials will need to be light, strong and capable of tolerating high temperatures. Carbon fiber is a material that can satisfy such requirements. Carbon-fiber sails can have very small areal mass density and are immune to UV degradation and can withstand high temperatures. Such a carbon fiber material, manufactured by Energy Science Laboratories Inc. of San Diego was fabricated by "node-bonding" 10 /spl mu/m diameter carbon fibers. To employ these carbon fiber microtruss materials efficiently for thrust and attitude control, it is useful to understand the electromagnetic response of these structures and compute the force exerted on them.
Keywords
carbon fibres; electromagnetic field theory; electromagnetic forces; solar radiation; space vehicles; 10 micron; UV degradation immunity; areal mass density; carbon fiber gossamer; electromagnetic emissions; electromagnetic response; high temperatures; microtruss materials; node-bonding; radiation force; solar sails; space sailcraft; Aircraft manufacture; Carbon dioxide; Electromagnetic forces; Electromagnetic launching; Electromagnetic radiation; Fiber lasers; Optical materials; Organic materials; Sun; Temperature;
fLanguage
English
Publisher
ieee
Conference_Titel
Antennas and Propagation Society International Symposium, 2001. IEEE
Conference_Location
Boston, MA, USA
Print_ISBN
0-7803-7070-8
Type
conf
DOI
10.1109/APS.2001.960098
Filename
960098
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