Thrust and thrust-to-power ratio in electrohydrodynamic propulsion electrode systems

被引：4

作者：

Dremin, D. V. ^{[1
]}

Khomich, V. Yu ^{[1
]}

Rebrov, I. E. ^{[1
]}

机构：

[1] RAS, Inst Electrophys & Elect Power, Dvorzovaya Naberezhnaya 18, St Petersburg 191186, Russia

来源：

INTERNATIONAL CONFERENCE - THE PHYSICS OF LOW TEMPERATURE PLASMA (PLTP-2017) | 2017年 / 927卷

关键词：

D O I：

10.1088/1742-6596/927/1/012015

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：

The influence on thrust parameter and efficiency from geometric parameters and design features of the ionocraft electrode is considered, dependences were obtained. The most effective mode of work lifters of the considered structures is achieved at low current. The increase of distance between the corona electrode and the collector gives the growth of thrust and thrust-to-power ratio up to some distance. It is advisable to use emitters with smaller diameter to reduce losses to the formation of the corona.

引用

页数：5

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