AEROSPACE SHANGHAI, Volume. 41, Issue 3, 130(2024)

Research Progress on the Working Mechanism of Ionic Liquid Electrospray Thrusters

Yuxiang CHEN*... Yufeng CHENG, Jinrui ZHANG, Guangchuan ZHANG, Haibin TANG and Weizong WANG |Show fewer author(s)
Author Affiliations
  • School of Astronautics, Beihang University, Beijing102206, China
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    Figures & Tables(11)
    Working principle of ionic liquid electrospray thrusters
    Prototypes of the array-type ionic liquid electrospray thruster
    Prototypes of the ionic liquid electrospray thrusters developed by the research institutions in China
    Three working processes of an ionic liquid electrospray thruster: cone jet, beam, and plume
    Emission modes of electrospray under different dimensionless numbers[44]
    Various emission modes of electrospray[53]
    Structure of the hybrid emitter ionic liquid electrospray thruster
    Phase diagram of the working mode for hybrid emitters[53]
    Beam structure of electrospray[44]
    Two neutralization modes of electrospray plumes[76]
    Half angles of plume divergence under different beam spacing[80]
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    Yuxiang CHEN, Yufeng CHENG, Jinrui ZHANG, Guangchuan ZHANG, Haibin TANG, Weizong WANG. Research Progress on the Working Mechanism of Ionic Liquid Electrospray Thrusters[J]. AEROSPACE SHANGHAI, 2024, 41(3): 130

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    Paper Information

    Category: Innovation and Exploration

    Received: Apr. 9, 2024

    Accepted: --

    Published Online: Sep. 3, 2024

    The Author Email:

    DOI:10.19328/j.cnki.2096-8655.2024.03.014

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