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Study of Asynchronous Solar Sail Deployment Using Finite Element Method.

Authors :
Yasuyuki MIYAZAKI
Go ONO
Kengo SHINTAKU
Yoji SHIRASAWA
Osamu MORI
Saburo MATUNAGA
Source :
Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan; 2014, Vol. 12 Issue ists 29, p63-67, 5p
Publication Year :
2014

Abstract

Solar sails are a form of spacecraft which deploys a large sail in space and uses solar radiation pressure for propulsion. IKAROS is a spinning solar sail developed by JAXA and was launched in 2010. As demonstrated with IKAROS, it is extremely effective to place various devices, such as thin-film solar cells for power generation, on the sail membrane of a solar sail. Such devices, however, contribute to the thickness of the sail, and may hinder the deployment of the sail. In this paper, the sail deployment method of IKAROS is reviewed and its dynamics, which may result in an asynchronous deployment of the sail, is investigated. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
18840485
Volume :
12
Issue :
ists 29
Database :
Complementary Index
Journal :
Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan
Publication Type :
Academic Journal
Accession number :
119557340