TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
Online ISSN : 1884-0485
ISSN-L : 1884-0485
c) Materials and Structures
Experiment and Analysis of Spinning Membrane Deployment Focusing on Shape Imbalance for Solar Sail
Kengo SHINTAKUSaburo MATUNAGAGo ONOHiraku SAKAMOTOTakeshi SATOHOsamu MORIYoji SHIRASAWANobukatsu OKUIZUMI
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2014 年 12 巻 ists29 号 p. Pc_55-Pc_62

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The small solar power sail demonstrator IKAROS was developed and launched in 2010 by JAXA and deployed its large membrane successfully. Through IKAROS's on-orbit operation, one of the most critical problems was a sail's shape imbalance during the sail deployment sequence. This paper focuses on the evaluation and consideration of the sail's imbalance through high vacuum experiments using a scale-down sail model. The experimental results obtained using the specially designed rotating mechanism and a small scale model lead to a hypothesis of the reason for the IKAROS's imbalanced deployment. The experimental results are extrapolated up to IKAROS's scale, using dimensionless analyses.
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© 2014 The Japan Society for Aeronautical and Space Sciences
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