ELECTROSPRAY

作品数：78被引量：172H指数：8
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Effect of ion solvation energy on electrohydrodynamic behavior of ionic liquid droplets in electrospray thrusters
《Chinese Journal of Aeronautics》2025年第3期222-233,共12页Yipeng FAN Chong CHEN Huifeng KANG Guangqing XIA Chang LU Yajie HAN 
supported by the National Key R&D Program of China(No.2020YFC2201100);the National Natural Science Foundation of China(Nos.12175032,12102082,12275044,12402327,12405290 and 12211530449);the Joint Program of the Science and Technology Program of Liaoning,China(No.2023JH2/101700285);the Fundamental Research Funds for the Central Universities of China(Nos.DUT22RC(3)078,DUT23RC(3)040 and DUT24ZD106);the S&T Program of Hebei,China(No.246Z2301G);the S&T Innovation Program of Hebei,China(Nos.SJMYF2022X18 and SJMYF2022X06);the Beijing Engineering Research Center of Efficient and Green Aerospace Propulsion Technology and Advanced Space Propulsion Laboratory of BICE,China(No.LabASP-2023-07).
The electrospray thruster supplied by ionic liquid is a promising micro-propulsion thruster with small size and precise thrust, which can emit both cations and anions to achieve self-neutralization. In order to furthe...
关键词：Ionic liquid ELECTROSPRAY ELECTROHYDRODYNAMICS Ion solvation energy Ion evaporation 
Axial emission characteristics of an ionic liquid electrospray thruster with a circular emitter被引量：1
《Chinese Journal of Aeronautics》2025年第1期297-305,共9页Cheng YANG Jiawei LUO Xiangbei WU Yan SHEN 
co-supported by the National Key R&D Program of China(No.2020YFC2201001);the Shenzhen Science and Technology Program,China(No.20210623091808026)。
Ionic Liquid Electrospray Thrusters(ILETs)are well suited for micro-nano satellite applications due to their small size,low power consumption,and high specific impulse.However,the limited thrust of a single-emitter IL...
关键词：ELECTROSPRAY Ionic liquid thruster Self-organize EMITTER Taylor cone 
Direct thrust test and asymmetric performance of porous ionic liquid electrospray thruster被引量：2
《Chinese Journal of Aeronautics》2023年第4期120-133,共14页Yuntao GUO Wei SUN Zhenning SUN Zhiwen WU Jianwu HE Chao YANG Ningfei WANG 
supported by the National Key R&D Program of China(No.2020YFC2201103).
In order to meet the demand of CubeSats for low power and high-performance micro-propulsion system,a porous ionic liquid electrospray thruster prototype is developed in this study.1010 conical emitter arrays are fabri...
关键词：Asymmetric performance Direct thrust test Ionic liquid electrospray thruster Time of flight mass spectrometry Torsional thrust stand 
Performance measurement and evaluation of an ionic liquid electrospray thruster被引量：4
《Chinese Journal of Aeronautics》2023年第3期1-15,共15页Chengjin HUANG Jianling LI Mu LI 
co-supported by NSAF,China(No.U1730134);the National Natural Science Foundation of China(No.11772310);the Innovation Foundation for Doctor Dissertation of Northwestern Polytechnical University,China(No.CX202034);the Innovation and Entrepreneurship Fund of the Student Affairs Department of Northwestern Polytechnical University,China(No.2021-CXCY-005)。
As a novel micro-propulsion system for small satellites(from micro to nano),the ionic liquid electro spray propulsion system is a promising candidate.However,performance measurement and evaluation of the Ionic Liquid ...
关键词：Electrospray thruster Ionic liquids Performance measurement Performance estimation MICRO-PROPULSION 
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