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电润湿离子液体电喷雾推力器原型的设计与性能

IF 1.7 4区 工程技术 Q2 ENGINEERING, AEROSPACE
Journal of Propulsion and Power Pub Date : 2023-11-30 DOI:10.2514/1.b39201
Wei Sun, Yuntao Guo, Zhiwen Wu, Zening Du, Ningfei Wang, Zhenning Sun
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引用次数: 0

摘要

推进与动力杂志，印刷前。
本文章由计算机程序翻译，如有差异，请以英文原文为准。
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Design and Performance of an Electrowetting Ionic Liquid Electrospray Thruster Prototype
Journal of Propulsion and Power, Ahead of Print.
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来源期刊
Journal of Propulsion and Power
Journal of Propulsion and Power 工程技术-工程：宇航
CiteScore
4.20
自引率
21.10%
发文量
97
审稿时长
6.5 months
期刊介绍： This Journal is devoted to the advancement of the science and technology of aerospace propulsion and power through the dissemination of original archival papers contributing to advancements in airbreathing, electric, and advanced propulsion; solid and liquid rockets; fuels and propellants; power generation and conversion for aerospace vehicles; and the application of aerospace science and technology to terrestrial energy devices and systems. It is intended to provide readers of the Journal, with primary interests in propulsion and power, access to papers spanning the range from research through development to applications. Papers in these disciplines and the sciences of combustion, fluid mechanics, and solid mechanics as directly related to propulsion and power are solicited.
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