云南高校图书馆联盟文献共享服务平台- ARCJET

ARCJET: 作品数：10被引量：17H指数：3; 导出分析报告; 相关领域：航空宇航科学技术理学更多>>; 相关作者：汤海滨戴梧叶刘宇刘岩松赵文华更多>>; 相关机构：北京航空航天大学清华大学更多>>; 相关期刊：《应用基础与工程科学学报》《Chinese Physics Letters》《Plasma Science and Technology》《Chinese Journal of Aeronautics》更多>>; 相关基金：国家自然科学基金更多>>

A three-dimensional numerical study on the effect of geometric asymmetry on arcjet thruster performance被引量：2: 《Plasma Science and Technology》2023年第5期131-146,共16页Hari Prasad NANDYALA Amit KUMAR Jayachandran THANKAPPAN; the Indian Space Research Organization(VSSC-ISRO)for funding this research through ISRO-IITM Cell。; In an arcjet thruster,the cathode and constrictor degrade with time,and the electrical arc discharge may become unsymmetrical.In this work,a three-dimensional numerical model of a hydrogen plasma arcjet is developed a...; 关键词：ARCJET geometric asymmetry 3D numerical modelling space electric propulsion HYDROGEN

Numerical simulation of hydrogen arcjet thruster with coupled sheath model: 《Plasma Science and Technology》2022年第2期145-161,共17页Deepak AKHARE Hari Prasad NANDYALA Jayachandran THANKAPPAN Amit KUMAR; supported by the Indian Space Research Organization(VSSC under grants ASE1415160ISROAMIK and ASE1718174ISROAMIK)。; In the present work,a complete 2D chemical and thermal non-equilibrium numerical model coupled with a relatively simple sheath model is developed for hydrogen arcjet thruster.Conduction heat transfer in the anode wall...; 关键词：ARCJET HYDROGEN numerical modeling plasma sheath space electric propulsion

Influences of characteristic parameters on starting-up process of an arcjet thruster: 《Chinese Journal of Aeronautics》2020年第12期3011-3017,共7页Yan SHEN Yinggang TONG Fuzhi WEI Zhaopu YAO Dawei HU; co-supported by the Defense Industrial Technology Development Program,China(No.JCKY2018203B029);the National Natural Science Foundation of China(No.11702021)。; Arcjet thruster has been a widely used electrical propulsion technology on GEO satellites since 1993.In its long history of technical development and commercial application,lifetime verification of an arcjet thruster ...; 关键词：Arc root ARCJET Electric propulsion Electrode ablation Starting-up process

Nonequilibrium modeling study on plasma flow features in a low-power nitrogen/hydrogen arcjet thruster被引量：3: 《Plasma Science and Technology》2017年第5期49-59,共11页何青松王海兴; Supported by National Natural Science Foundation of China(Grant Nos.11575019,11275021); Gasdynamic flow features in an electrothermal arcjet thruster with a mixture of 1：2 nitrogen/hydrogen as the working gas have been studied by a two-temperature numerical simulation.Seven species and 17 kinetic proces...; 关键词：plasma heat transfer and flow arcjet thruster chemical nonequilibrium

Spectroscopic Measurement of Shock Waves in an Arcjet Plasma Expanding Through a Conical Nozzle: 《Plasma Science and Technology》2013年第2期89-92,共4页K.KOZUE G.KUMAKAWA S.NAMBA T.ENDO K.TAKIYAMA K.SATO N.TAMURA; A diamond-shaped shock wave was created in a helium arcjet plasma. Visi- ble/ultraviolet emission spectroscopy was used to investigate the condition for the formation of stable shocks and to determine characteristics ...; 关键词：arcjet plasma shock wave plasma spectroscopy atomic and molecular pro-cesses

Modelling Study to Compare the Flow and Heat Transfer Characteristics of Low-Power Hydrogen,Nitrogen and Argon Arc-Heated Thrusters被引量：5: 《Plasma Science and Technology》2010年第6期692-701,共10页王海兴陈熙潘文霞 A.B.MURPHY 耿金越贾少霞; supported by National Natural Science Foundation of China (Nos.50836007, 10921062); A modelling study is performed to compare the plasma flow and heat transfer characteristics of low-power arc-heated thrusters （arcjets） for three different propellants： hydrogen, nitrogen and argon. The all-speed S...; 关键词：low-power arcjet plasma flow and heat transfer numerical modelling propellant-type effects

Effect of Nozzle Temperature on the Performance of a 1 kW H_2-N_2 Arcjet Thruster被引量：1: 《Plasma Science and Technology》2010年第4期473-477,共5页潘文霞黄河激吴承康; supported by National Natural Science Foundation of China (Nos.50836007, 10775164 and 10921062); A 1 kW-class arcjet thruster was fired in a vacuum chamber at a pressure of 18 Pa. A gas mixture of H2 ： N2 = 2.8 ： 1.5 in volume at a total flow rate of 4.3 slm was used as the propellant with an input power fixed ...; 关键词：arcjet thruster nozzle temperature energy conversion experimental measurement

Effects of Anode Temperature on Working Characteristics and Performance of a Low Power Arcjet Thruster被引量：2: 《Chinese Physics Letters》2009年第12期168-170,共3页潘文霞李腾吴承康; Supported by the National Natural Science Foundation of China under Grant Nos 10775164, 50836007 and 10621202.; An arc-heated thruster of 130-800W input power is tested in a vacuum chamber at pressures lower than 20Pa with argon or H2-N2 gas mixture as propellant. The time-dependent arc voltage-current curve, outside-surface te...

低功率电弧加热发动机的实验研究被引量：3: 《应用基础与工程科学学报》2002年第2期168-173,共6页陈黎明赵文华刘岩松; 进行了一种低功率电弧加热发动机 (Arcjet)的实验研究 .介绍了发动机的结构尺寸和材料选择 .实验系统包括真空模拟系统 ,供电系统 ,推进剂供给系统 ,参数测量系统和发动机本体 .在真空环境下 ,用氩作推进剂 ,得到了不同工况下发动机的...; 关键词：小卫星推进系统电弧加热发动机 ARCJET 低功率

小功率电弧等离子体发动机试验及性能研究被引量：3: 《中国空间科学技术》2000年第6期57-61,68,共6页汤海滨刘宇戴梧叶; 国家教委"2 11"工程项目; 电推进技术已应用于航天的多个领域 ,电弧等离子体发动机 (Arcjet)因其高比冲、高推力 /功率比以及大的推进剂选择范围等特点成为当前国际上电火箭研究和应用的热点。文章总结小功率 Arcjet实验及性能研究 ,介绍了实验研究系统的主要组...; 关键词：电弧等离子体发动机实验设备性能参数 ARCJET

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