Laboratory Facility for Simulating Solar Wind Sails

被引:0
|
作者
Funaki, Ikkoh [1 ,5 ]
Ueno, Kazuma [2 ]
Oshio, Yuya [2 ]
Ayabe, Tomohiro [3 ]
Horisawa, Hideyuki [3 ]
Yamakawa, Hiroshi [4 ,5 ]
机构
[1] Japan Aerosp Explorat Agcy, Sagamihara, Kanagawa 2298510, Japan
[2] Grad Univ Adv Studies, Sagamihara, Kanagawa 2298510, Japan
[3] Tokai Univ, Kanagawa 2591292, Japan
[4] Kyoto Univ, Kyoto 6110011, Japan
[5] Japan Sci & Technol Agcy, CREST, Kawaguchi, Saitama 3320012, Japan
来源
RAREFIED GAS DYNAMICS | 2009年 / 1084卷
关键词
Plasma sail; Magnetic sail; Spacecraft propulsion; Arcjet; Laboratory Astrophysics; SPACECRAFT PROPULSION;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Magnetic sail (MagSail) is a deep space propulsion system, in which an artificial magnetic cavity captures the energy of the solar wind to propel a spacecraft in the direction leaving the sun. For a scale-model experiment of the plasma flow of MagSail, we employed a magnetoplasmadynamic arcjet as a solar wind simulator. It is observed that a plasma flow from the solar wind simulator reaches a quasi-steady state of about 0.8 ms duration after a transient phase when initiating the discharge. During this initial phase of the discharge, a blast-wave was observed to develop radially in a vacuum chamber. When a solenoidal coil (MagSail scale model) is immersed into the quasi-steady flow where the velocity is 45 km/s, and the number density is 10(19) m-3. a bow shock as well as a magnetic cavity were formed in front of the coil. As a result of the interaction between the plasma flow and the magnetic cavity, the momentum of the simulated solar wind is decreased, and it is found from the thrust measurement that the solar wind momentum is transferred to the coil simulating MagSail.
引用
收藏
页码:754 / +
页数:2
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