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Magnetohydrodynamic Analysis of Magnetoplasma Sail Considering Thermal Pressure and Dynamic Pressure
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- Murayama Yuki
- 連絡先著者(Corresponding author):yuki.murayama@ac.jaxa. jp 総合研究大学院大学
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- Hara Ryota
- 総合研究大学院大学
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- Yamagiwa Yoshiki
- 静岡大学
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- Oshio Yuya
- 龍谷大学
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- Nishida Hiroyuki
- 東京農工大学
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- Funaki Ikkoh
- 宇宙航空研究開発機構
Bibliographic Information
- Other Title
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- 静圧と動圧を考慮した磁気プラズマセイルの電磁流体解析
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Description
<p>Magsail is a space propulsion system using the interactions between the solar wind and the magnetic field generated by the onboard coils. Magnetoplasma sail is a propulsion system that increases thrust by expanding the magnetosphere through plasma injection from the spacecraft. There are two mechanisms on the magnetospheric inflation: method using frozen-in of magnetic field to carry magnetic field lines by high dynamic pressure plasma and method using the diamagnetic current by thermal plasma, which is called the ring current. We investigated the effect of the dynamic pressure and thermal pressure on the MPS thrust performance used electromagnetic hydrodynamic simulation. It was shown that the ring current is enhanced by adding dynamic pressure to the thermal plasma and increases thrust gain. The high thrust gain over 2.25 was obtained at βth = 0.5 - 2 and βk = 4 - 8. However, the thrust is reduced because the super magneto acoustic wave region is generated in the magnetosphere, which prevents the propagation of thrust in large β conditions. The wide parameter survey reveals injection plasma parameter regions where thrust reduction is restrained and high thrust gain is obtained. </p>
Journal
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- JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 71 (2), 67-77, 2023
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
- 1390858608268657792
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- ISSN
- 24323691
- 13446460
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- Text Lang
- ja
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- Data Source
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- JaLC
- Crossref
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- Abstract License Flag
- Disallowed