Thrust and Attitude Evaluation of Magnetic Sail by Three-Dimensional Hybrid Particle-in-Cell Code

被引：14

作者：

Kajimura, Yoshihiro ^{[1
]}

Funaki, Ikkoh ^{[2
]}

Matsumoto, Masaharu ^{[3
]}

Shinohara, Iku ^{[2
]}

Usui, Hideyuki ^{[3
]}

Yamakawa, Hiroshi ^{[4
]}

机构：

[1] Akashi Natl Coll Technol, Dept Elect & Comp Engn, Akashi, Hyogo 6758501, Japan

[2] Japan Aerosp Explorat Agcy, Inst Space & Astronaut Sci, Sagamihara, Kanagawa 2525210, Japan

[3] Kobe Univ, Grad Sch Syst Informat, Dept Computat Sci, Kobe, Hyogo 6578501, Japan

[4] Kyoto Univ, Kyoto 6110011, Japan

来源：

JOURNAL OF PROPULSION AND POWER | 2012年 / 28卷 / 03期

基金：

日本科学技术振兴机构;

关键词：

PLASMA SAIL; SIMULATION;

D O I：

10.2514/1.B34334

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A magnetic sail generates a propulsive force using the interaction between the solar wind and an artificial magnetosphere generated by a hoop coil. To investigate the electromagnetic thrust characteristics of the magnetic sail, such as the values of the drag, lift, transverse force, and pitching moment, three-dimensional hybrid (ion particle and electron fluid) particle-in-cell simulations are conducted in the range from the ion inertial scale to the magnetohydrodynamic scale. The drag values calculated in the different magnetic moment directions to the solar wind flow direction agree to within a factor of 2. The attitude of spacecraft is stable when the magnetic moment vector is perpendicular to the solar wind flow direction. It is found that these two results do not depend on the size of the magnetosphere.

引用

页码：652 / 663

页数：12

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