Study on the control of propellant flow by electric field in ionic liquid electrospray thruster-Reference-Cited by-同舟云学术

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Study on the control of propellant flow by electric field in ionic liquid electrospray thruster

Published:2022-02 Issue: Volume:183 Page:121926
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

Sun Wei,Wu Zhiwen,Sun Zhenning,Guo Yuntao,Huang Tiankun,Sun Guorui,Xue Jingran,Wang Ningfei

Funder

National Key Research and Development Program of China

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference28 articles.

1. The technological and commercial expansion of electric propulsion;Lev;Acta Astronaut.,2019

2. CubeSat constellation management using Ionic Liquid Electrospray Propulsion;Jenkins;Acta Astronaut.,2018

3. Ionic liquid electrospray behavior in a hybrid emitter electrospray thruster;Zhang;Int. J. Heat Mass Transf.,2021

4. Molecular dynamics simulation of ionic liquid electrospray: revealing the effects of interaction potential models;Zhang;Acta Astronaut.,2021

5. Experimental investigation on current modes of ionic liquid electrospray from a coned porous emitter;Huang;Acta Astronaut.,2021

Cited by 8 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Molecular dynamics simulation on external wetted ionic liquid electrospray considering the asymmetric wetting behavior of cations and anions;Journal of Molecular Liquids;2024-09

2. Study on the plume self-neutralization of ionic liquid electrospray thruster based on median potential;Plasma Sources Science and Technology;2024-05-01

3. Study on the control of electrowetting and permeation of ionic liquids on porous substrates via molecular dynamics simulations;Journal of Molecular Liquids;2024-05

4. Preliminary study of the electrospray DPE peculiarities from the liquid surface in the presence of the CSWs;Plasma Science and Technology;2023-12-13

5. Design and Performance of an Electrowetting Ionic Liquid Electrospray Thruster Prototype;Journal of Propulsion and Power;2023-11-30

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