Numerical Model for Pure Magnetic Sail
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- ASHIDA Yasumasa
- 京都大学生存圏研究所
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- FUNAKI Ikkoh
- 宇宙航空研究開発機構宇宙科学研究所
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- YAMAKAWA Hiroshi
- 京都大学生存圏研究所
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- KAJIMURA Yoshihiro
- 宇宙航空研究開発機構宇宙科学研究所
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- KOJIMA Hirotsugu
- 京都大学生存圏研究所
Bibliographic Information
- Other Title
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- 磁気セイル推力解析のための簡易モデルの検討
- ジキ セイルスイリョク カイセキ ノ タメ ノ カンイ モデル ノ ケントウ
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Abstract
The magnetic sail is a spacecraft propulsion system using the interaction between the magnetic field and the solar wind. In this paper, to evaluate the propulsive force generated by a Pure Magnetic Sail spacecraft, a new numerical analysis model including the ion's finite Larmor-radius effect is proposed. In this analysis model, the trajectories of ion particles are solved based on the Flux-Tube model and electrons are treated as a plasma fluid under the assumption of quasi-neutrality and steady state. As for the electromagnetic field, the induction equation is employed to obtain a steady electromagnetic field. Using the Flux-Tube model, a 500-km-size magnetosphere was found to produce a thrust level of 1500N when a magnetic moment of the magnetic sail is set to 3.9×1016Wbm. This thrust level agrees well with the result obtained by magnetohydrodynamics model (1600N) and that by Hybrid particle-in-cell model including ion kinetic effects (1560N). Also, the computational cost of the Flux-Tube model is reduced to about 1/10 of that of Hybrid-PIC model.
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 59 (688), 126-131, 2011
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Keywords
Details 詳細情報について
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- CRID
- 1390001204469604608
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- NII Article ID
- 10029831480
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- NII Book ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL BIB ID
- 11127644
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
- KAKEN
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- Abstract License Flag
- Disallowed