Scale-model experiment of magnetoplasma sail for future deep space missions

被引:0
|
作者
Funaki, Ikkoh [1 ]
Yamakawa, Hiroshi [2 ]
Ueno, Kazuma [3 ]
Kimura, Toshiyuki [3 ]
Ayabe, Tomohiro [3 ]
Horisawa, Hideyuki [3 ]
机构
[1] Japan Aerosp Explorat Agcy, Sagamihara, Kanagawa 2298510, Japan
[2] Kyoto Univ, Uji, Kyoto 6110011, Japan
[3] Tokai Univ, Hiratsuka, Kanagawa 2591292, Japan
来源
BEAMED ENERGY PROPULSION | 2008年 / 997卷
关键词
plasma sail; Magnetic sail; spacecraft propulsion; arcjet; laboratory astrophysics;
D O I
暂无
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
When Magnetic sail (MagSail) spacecraft is Operated in space, the supersonic solar wind plasma flow is blocked by an artificially produced magnetic cavity to accelerate the spacecraft in the direction leaving the Sun. To evaluate the momentum transferring process from the solar wind to the coil onboard the MagSail spacecraft, we arranged a laboratory experiment of MagSail spacecraft. Based on scaling considerations, a solenoidal coil was immersed into the plasma flow from a magnetoplasmadynamic arcjet in a quasi-steady mode of about 1 ms duration. In this setup, it is confirmed that a magnetic cavity, which is similar to that of the geomagnetic field, was formed around the coil to produce thrust in the ion Larmor scale interaction. Also, the controllability of magnetic cavity size by a plasma jet from inside the coil of MagSail is demonstrated, although the thrust characteristic of the MagSail with plasma jet, which is so called plasma sail, is to be clarified in our next step.
引用
收藏
页码:553 / +
页数:2
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