Characteristics of Ion-Ion Thruster Generating Continuously Positive and Negative Ion Beams

被引:6
|
作者
Koda, Daiki [1 ]
Kuninaka, Hitoshi [2 ]
Tsukizaki, Ryudo [2 ]
机构
[1] Japan Aerosp Explorat Agcy, Space Explorat Innovat Hub Ctr, Sagamihara, Kanagawa 2525210, Japan
[2] Japan Aerosp Explorat Agcy, Dept Space Flight Syst, Sagamihara, Kanagawa 2525210, Japan
关键词
Positive ions;
D O I
10.2514/1.B37166
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The neutralizers in ion thruster systems do not generate thrust force. Hence, the power consumption of a neutralizer limits the thrust efficiency of the ion thruster system. Therefore, an ion thruster system is proposed that uses a negative ion source that generates thrust force as well as neutralizes the positive ion beam. In this study, in order to verify the feasibility of this ion thruster system by ground experiments, a negative fullerene ion source was developed and three experiments were conducted. First, in order to demonstrate that the satellite can accelerate ions without becoming charged, the positive and negative ion beams were accelerated in the floating condition using a feedback circuit. Second, in order to verify whether the formation of the virtual anode could be suppressed, the space potential and the beam profile in the downstream region of the ion beam were measured. Third, in order to demonstrate that the thruster system generates thrust force, the thrust with a beam target was measured. From the aforementioned results, it was concluded that the experimental verification of the feasibility of the ion thruster with combined positive and negative ions without a neutralizer was successful.
引用
收藏
页码:565 / 571
页数:7
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