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- UENO Kazuma
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- OSHIO Yuya
- Department of Space and Astronautical Science, The Graduate University for Advanced Studies (Sokendai)
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- FUNAKI Ikkoh
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- HORISAWA Hideyuki
- Department of Aeronautics and Astronautics, Tokai University
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- YAMAKAWA Hiroshi
- Research Institute for Sustainable Humanosphere, Kyoto University
Abstract
Magnetic Sail, which generates thrust by utilizing the interaction between the artificial magnetic field and the solar wind plasma stream, is next generation propulsion for deep space exploration. In this study, thrust of Magnetic Sail scale model, which correspond to 10 N-class Magnetic Sail in space, for various tilt angles were measured with the parallelogram-pendulum thrust stand. The magnetospheric size L=0.1 m (60 Am2 of magnetic moment) of Magnetic Sail was demonstrated and measured thrust for tilt angle 0 degrees (dipole-moment perpendicular to the plasma flow) was about 1.2 N which correspond to 10 N-class Magnetic Sail in space. Thrust increase with increasing of tilt angles and was about 1.5 times as large as that of 0 degrees case in the case of 90 degrees.
Journal
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 10 (ists28), Tb_13-Tb_16, 2012
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390282680296494592
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- NII Article ID
- 130003301059
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- ISSN
- 18840485
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- Text Lang
- en
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- Data Source
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- JaLC
- Crossref
- CiNii Articles
- KAKEN
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- Abstract License Flag
- Disallowed