Miniaturized Plasma Sources: Can Technological Solutions Help Electric Micropropulsion?

被引：10

作者：

Baranov, Oleg O. ^{[1
]}

Xu, Shuyan ^{[2
]}

Xu, Luxiang ^{[2
]}

Huang, S. ^{[2
]}

Lim, J. W. M. ^{[2
]}

Cvelbar, U. ^{[3
]}

Levchenko, Igor ^{[2
,4
]}

Bazaka, Kateryna ^{[4
]}

机构：

[1] Natl Aerosp Univ, Fac Aircraft Engines, UA-61183 Kharkov, Ukraine

[2] Nanyang Technol Univ, Plasma Sources & Applicat Ctr, NIE, Singapore 637616, Singapore

[3] Jozef Stefan Inst, Dept Surface Engn & Optoelect, Ljubljana 1000, Slovenia

[4] Queensland Univ Technol, Sch Chem, Phys, Mech Engn, Brisbane, Qld 4000, Australia

来源：

IEEE TRANSACTIONS ON PLASMA SCIENCE | 2018年 / 46卷 / 02期

基金：

新加坡国家研究基金会;

关键词：

Microplasma; plasma sources; propulsion; MICROPLASMAS; PROPULSION; DEVICES;

D O I：

10.1109/TPS.2017.2773073

中图分类号：

O35 [流体力学]; O53 [等离子体物理学];

学科分类号：

070204 ; 080103 ; 080704 ;

摘要：

In this paper, we examine several different types of miniaturized plasma sources that have been developed for nonpropulsion applications, but could be useful for the advancement of electric propulsion. With the same or similar physical principles and often similar design solutions, such sources suggest useful pathways for modernization and integration of presently available well established as well as emerging miniaturized plasma sources into space thruster systems. Features related to miniaturization and optimization of the technological plasma sources will provide useful insights for consideration by the electric propulsion specialists. It is not the aim of this paper to show an entire spectrum of technological microplasma systems, but rather to outline possible future trends and perspectives for the miniaturized technological plasmas in relation to space micropropulsion systems.

引用

页码：230 / 238

页数：9

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