日本航空宇宙学会論文集
Online ISSN : 2432-3691
Print ISSN : 1344-6460
ISSN-L : 1344-6460
論文
磁気プラズマセールによる外惑星探査
山川 宏小川 博之藤田 和央野中 聡澤井 秀次郎國中 均船木 一幸大津 広敬中山 宜典
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2004 年 52 巻 603 号 p. 148-152

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A magneto-plasma sail produces the propulsive force due to the interaction between the artificial magnetic field around a spacecraft inflated by the plasma and the solar wind erupted from the Sun. The inflation of the magnetic field by the plasma was proposed by a group of the University of Washington and the basic research has just started. This paper summarizes the characteristics of the magneto plasma sail by comparing with the other low-thrust propulsion systems, and investigates its potential application to near future planetary missions. Finally, an engineering satellite to demonstrate the magneto-plasma sail is proposed as a first step.

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© 2004 The Japan Society for Aeronautical and Space Sciences
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