Performance of Dimethyl Ether Arcjet Thrusters and Its Dependence on Electrode Configurations

被引:0
|
作者
Kakami, Akira [1 ]
Beppu, Shinji [1 ]
Maiguma, Muneyuki [1 ]
Tachibana, Takeshi [1 ]
机构
[1] Kyushu Inst Technol, Dept Mech Engn, Kitakyushu, Fukuoka 8048550, Japan
关键词
D O I
10.2514/1.58455
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper discusses an arcjet thruster using dimethyl ether propellant. Dimethyl ether is an ether compound having no toxicity and relatively weak reactivity to materials and is storable in a liquid form without complex temperature management, because it has a vapor pressure of 0.6 MPa at 273 K. In this study, a dimethyl ether arcjet thruster was prototyped and tested to evaluate its performance: specific impulse and thruster efficiency. Flat-type cathodes of 2 and 4 mm in diameter were designed to investigate the influence of cathode diameter and electrode gap on performance. Thrust measurements showed that a dimethyl ether arcjet thruster with a cathode of 2 mm in diameter set at a 2 mm electrode gap yielded the best specific impulse of 400 s and a thruster efficiency of 0.17.
引用
收藏
页码:603 / 608
页数:6
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