Experimental approach to improve ion thruster performance: Part 1 - Effects of the propellant delivery method

被引：0
|
作者：
Okawa, Y [1 ]
Takegahara, H [1 ]
机构：
[1] Tokyo Metropolitan Inst Technol, Dept Aerosp Engn, Tokyo, Japan
来源：
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 1999年 / 42卷 / 137期
关键词：
electric propulsion; ion thruster; experiment; propellant feed;
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：141 / 143
页数：3
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