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THRUSTER: 作品数：91被引量：146H指数：6; 导出分析报告; 相关领域：航空宇航科学技术更多>>; 相关作者：黄先科胡伟陈健毛根旺陈君更多>>; 相关机构：西北工业大学北京控制工程研究所更多>>; 相关期刊：更多>>; 相关基金：国家自然科学基金国家高技术研究发展计划中国博士后科学基金国家重点基础研究发展计划更多>>

Design and experimental study of a field-reversed configuration plasma thruster prototype: 《Plasma Science and Technology》2025年第3期118-126,共9页Yuxuan HUANG Ming ZHANG Yong YANG Fangwei LYU Xiaopeng YI Chaofan LYU Yisong ZHANG Bo RAO; supported by National Natural Science Foundation of China (NSFC) (Nos.62201217 and 51821005)。; The field-reversed configuration(FRC)plasma thruster driven by rotating magnetic field(RMF),abbreviated as the RMF-FRC thruster,is a new type of electric propulsion technology that is expected to accelerate the deep s...; 关键词：rotating magnetic field(RMF) field-reversed configuration(FRC) plasma thrusters plasma current

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

A study of an air-breathing electrodeless plasma thruster discharge: 《Propulsion and Power Research》2024年第4期459-474,共16页J.Zhou F.Taccogna P.Fajardo E.Ahedo; funded initially by the HIPATIA project of HORIZON 2020(European Commission),Grant No.GA870542;completed with funding from the SUPERLEO project(Agencia Estatal de Investigación,Spanish Government),Grant No.TED2021-132484B-I00;The stay of J.Zhou at ISTP-CNR is being supported by the program Recualificación del Sistema Universitario Español,Margarita Salas,of the Ministerio de Universidades(Spanish Government)。; Plasma chemistry of main Earth atmospheric components in VLEOs is implemented in a hybrid 2D axisymmetric simulation code to assess the air-breathing concept in an electrodeless plasma thruster.Relevant electron-heavy...; 关键词：Atmosphere-breathing electric propulsion In-space propulsion Electrodeless plasma thrusters Modeling and simulation Molecular propellants

Thrust estimate method of an on-orbit Hall thruster using Hall drift current: 《Plasma Science and Technology》2024年第12期150-159,共10页Ziying REN Liqiu WEI Zexin LIU Yanlin HU Liang HAN Hong LI Yongjie DING Xiufeng ZHONG; funded by the Basic Research on National Defense of China(No.JCKY2021603B033),which is gratefully acknowledged。; In order to realize the thrust estimation of the Hall thruster during its flight mission,this study establishes an estimation method based on measurement of the Hall drift current.In this method,the Hall drift current...; 关键词：thrust estimation Hall effect thruster Hall drift current inverse problem Tikhonov regularization

Numerical Analysis of the Hydrodynamic Performance Impact of Novel Appendage on Rim-driven Thruster: 《哈尔滨工程大学学报(英文版)》2024年第4期762-775,共14页Hengxu Yang Dongqin Li Feng Zhang; Addressing the ongoing challenge of enhancing propulsion efficiency in rim-driven thrusters(RDTs),a novel energy-saving appendage was designed to mitigate energy dissipation and improve efficiency.Computational fluid ...; 关键词：Rim-driven thruster Novel appendage Computational fluid dynamics Moving reference frame methodology Propulsion efficiency

Design of bionic water jet thruster with double-chamber driven by electromagnetic force: 《International Journal of Mechanical System Dynamics》2024年第3期292-302,共11页Chong Cao Yasong Zhang Chengchun Zhang Chun Shen Wen Cheng Zhenjiang Wei Zhengyang Wu Luquan Ren; National Key Research and Development Program of China,Grant/Award Number:2018YFA0703300;National Natural Science Foundation of China,Grant/Award Numbers:52275289,51875243,52305306;Jilin Scientific and Technological Development Program,Grant/Award Number:20220508144RC;Taishan Industrial Experts Program。; In response to the limitations of the single-chamber water jet thruster used in underwater vehicles mimicked by natural cephalopods,a novel approach involving a double-chamber water jet thruster has been proposed.This...; 关键词：water jet thruster DIAPHRAGM electromagnetic force

Full lifetime demonstration of a Micro-Cathode-Arc thruster evolution characteristics: 《Chinese Journal of Aeronautics》2024年第6期38-49,共12页Zhe ZHANG Zijing ZHAO Xiangyang LIU Ningfei WANG; supported by the National Natural Science Foundation of China(No.52177128).; Ground lifetime test is the most crucial experiment to assess the performance,reliability.and flight qualification of electric propulsion,and it can bring new insights for understanding the operation characteristics.T...; 关键词：Electric propulsion Lifetime test Micro-Cathode-Arc Thruster(uCAT) Conductive film Discharge characteristics Plasma parameters

Controlled flight of a self-powered micro blimp driven by insect-sized flapping-wing thrusters: 《Chinese Journal of Aeronautics》2024年第6期127-136,共10页Xian YU Zhiwei LIU Jiaming LENG Mingjing QI Xiaojun YAN; co-supported by the Beijing Natural Science Foundation,China(No.3232010);the National Natural Science Foundation of China(No.12002017);the Ministry of Education of the People’s Republic of China 111 Project(No.B08009).; Micro aerial platforms face significant challenges in achieving long controlled endurance as most of the energy is consumed to overcome the weight of the body.In this study,we present a controllable micro blimp that a...; 关键词：Microairvehicle Aircraft control Self-powered micro blimp Flapping-wing thruster Wireless flight

Experimental investigation of the polarityswitching process with different bipolar ionic liquid thruster operating frequencies: 《Plasma Science and Technology》2024年第6期1-13,共13页吴湘蓓杨铖罗嘉伟沈岩; co-supported by the National Key R&D Program of China(No.2020YFC2201001);the Shenzhen Science and Technology Program(No.20210623091808026).; The bipolar ionic liquid thruster employs ionic liquid as a propellant to discharge positively and negatively charged high-energy particles under an alternating current(AC)power source,effectively suppressing electroc...; 关键词：space electric propulsion ionic liquid thruster bipolar operation mode FREQUENCY

Structure Design of Underwater Micro Robot: 《Modern Mechanical Engineering》2024年第1期12-24,共13页Md Shahriar Sujan Joy Howlader Md Jahangir Alam Md Al Imran Tapu; A submergible robot model has been presented, and for 3D printing measures, their parts have been modified enough. It has been shown in our design that using printable connectors—a few engines and weight arrangements...; 关键词：Submergible Robot THRUSTER ADAPTER Raspberry Pi 3D Printer Open Source Software

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