云南高校图书馆联盟文献共享服务平台- MAGNETOPLASMA

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Temporal variation characteristics of cathode temperature in a magnetoplasmadynamic thruster: 《Chinese Physics B》2025年第2期334-340,共7页Cheng Zhou Peng Wu Yun-Tao Song Jin-Xing Zheng Yong Li Ge Wang Hai-Yang Liu; The magnetoplasmadynamic thruster(MPDT) is characterized by its high specific impulse and substantial thrust density, making it a promising propulsion system for deep space exploration missions. In both laboratory exp...; 关键词：magnetoplasmadynamic thruster(MPDT) optical diagnostic monochromatic radiation cathode temperature

Experimental study on performance of 100-kW low temperature superconducting steady-state magnetoplasmadynamic thruster: 《Chinese Physics B》2025年第2期328-332,共5页Cheng Zhou Peng Wu Yun-Tao Song Jin-Xing Zheng Yong Li Ge Wang Hai-Yang Liu; Applied field magnetoplasmadynamic thrusters(AF-MPDTs), with their high specific impulse and considerable thrust, are increasingly favored for large-scale space missions. This paper presents the composition, functiona...; 关键词：magnetoplasmadynamic thruster high-power electric propulsion superconduction performance measurements

Hēki:A superconducting magnet for space propulsion on the International space Station-Pathfinder design and experimental thermal testing: 《Superconductivity》2024年第4期59-76,共18页Jamal Olatunji Nicholas Strickland Max Goddard-Winchester Benjamin Mallett Celine Jane Cameron Shellard Emile Webster Betina Pavri Avinash Rao Randy Pollock; funded by the New Zealand Ministry of Business,Inno-vation and Employment(contract number RTVU2003).; Applied‐field magnetoplasmadynamic(AF‐MPD)thrusters are a high‐power electric propulsion solution for satellites and spacecraft,offering high efficiency,high specific impulse and high thrust density.The integration...; 关键词：Electric Propulsion Satellite Propulsion Magnetoplasmadynamic Thrusters Flux Pumps SPACE

Endurance-test and theoretical prediction of a rare earth nanocathode for the applied field magnetoplasmadynamic thruster: 《Plasma Science and Technology》2023年第10期49-59,共11页王戈李永周成魏延明孔春才郑学程张心霨杨志懋郑金星丛云天王宝军; The erosion loss of cathode is essential for the lifetime of magnetoplasmadynamic thruster(MPDT).In this work,an endurance test system for MPDT cathodes was designed and developed,and the erosion characteristics,erosi...; 关键词：magnetoplasma dynamic thruster nano-oxide cathode ablation models

Simulation of a helicon plasma source in a magnetoplasma rocket engine: 《Plasma Science and Technology》2022年第7期53-62,共10页Zhenyu YANG Wei FAN Jianguo WEI Xianwei HAN; supported by the Shaanxi Key Laboratory of Plasma Physics and Applied Technology。; The helicon plasma source,which generates high thrust and high impulse,is of vital importance for magnetoplasma rocket engines.In this work,a multi-component,two-dimensional,axisymmetric fluid model coupled with an el...; 关键词：space propulsion MPRE helicon plasma source discharge mode conversion

A semiclassical approach to surface Fermi arcs in Weyl semimetals被引量：1: 《Science China(Physics,Mechanics & Astronomy)》2022年第6期110-115,共6页Jiajia Huang Luyang Wang Dao-Xin Yao; supported by the National Key Research and Development Program of China(Grant Nos.2017YFA0206203,and 2018YFA0306001);the National Natural Science Foundation of China(Grant Nos.12004442,11974432,and 92165204);the Guangdong Basic and Applied Basic Research Fund(Grant No.2019A1515011337);the Shenzhen International Quantum Academy(Grant No.SIQA202102);the Leading Talent Program of Guangdong Special Projects(Grant No.201626003)。; We present a semiclassical explanation for the morphology of the surface Fermi arcs of Weyl semimetals.Viewing the surface states as a two-dimensional Fermi gas subject to band bending and Berry curvatures,we show tha...; 关键词：Weyl semimetals surface Fermi arcs semiclassical equations of motion Dirac semimetals surface magnetoplasma

MARSZUG—A Space Train for Regular Delivery of Astronauts onto Mars: 《Advances in Aerospace Science and Technology》2021年第2期93-113,共21页Alexander Rubinraut; A project of the space train MARSZUG intended for regular delivery of astronauts to Mars is considered. In the first stage of the flight, the astronauts with the help of the carrier rocket equipped with a chemical roc...; 关键词：MARS MARS-K Combined Propulsion System MARS-K Superconductive Magnetoplasma Electrorocket Engine Takeoff-Landing Capsule Space Refueler

Cathode erosion site distributions in an applied-field magnetoplasmadynamic thruster被引量：4: 《Plasma Science and Technology》2020年第9期59-65,共7页Peng WU Yibai WANG Yong LI Baojun WANG Kaiyu ZHANG Haibin TANG Jinbin CAO; supported by the Fundamental Research Program(No.11872093)。; Erosion can influence cathode life,and is thus considered to be one of the main factors limiting the application of applied-field magnetoplasmadynamic thrusters.In this paper,erosion sites on graphite cathodes are stu...; 关键词：electric propulsion applied-field magnetoplasmadynamic thruster cathode erosion magnetic field propellant mass flow rate

Moonplane—A Spacecraft for Regular Delivery of Astronauts onto the Moon被引量：1: 《Advances in Aerospace Science and Technology》2019年第3期43-56,共14页Alexander Rubinraut; A project of spacecraft “moonplane” for regular delivery of astronauts onto the Moon is considered. At the first stage of flight by using a carrier rocket, equipped with a chemical rocket engine, the astronauts are ...; 关键词：Moonplane Superconducting MAGNETOPLASMA Electrorocket Engine MARS Interorbital MODULE LUNAR MODULE Solar Battery of GALLIUM ARSENIDE

On the dielectric response function and dispersion relation in strongly coupled magnetized dusty plasmas被引量：1: 《Chinese Physics B》2018年第10期465-470,共6页M Shahmansouri N Khodabakhshi; Using the generalized viscoelastic fluid model, we derive the dielectric response function in a strongly coupled dusty magnetoplasma which reveals two different dust acoustic（DA） wave modes in the hydrodynamic and k...; 关键词：dusty plasma strongly coupled plasma MAGNETOPLASMA dielectric response function

MAGNETOPLASMA