| [1]靳旭红，黄飞，张俊，等.上层大气层飞行器研究进展及气动技术挑战[J].航空学报, 2024, 45(22):030254-030254[2]JIN X H， HUANG F， ZHANG J， et al.Spacecraft in upper atmosphere： Research development and aerodynam-ic challenges[J].Acta Aeronautica et Astronautica Sinica, 2024, 45(22):030254-030254[3]郑鹏, 吴建军, 张宇, 等.用于吸气式电推进系统的射频等离子体推力器实验测试[J].航空学报, 2024, 45(21):130144-130144[4]ZHENG P, WU J J, ZHANG Y, et al.Experimental testing of inductively coupled radiofrequency plasma thruster for at-mosphere-breathing electric propulsion system[J].Acta Aer-onautica et Astronautica Sinica, 2024, 45(21):130144-130144[5] Herdrich G, Papavramidis K, Maier P, et al.Platform and system design study of a VLEO satellite platform using the IRS RF Helicon-based Plasma Thruster[C]//Proceedings of the 73rd International Astronautical Congress. International Astronautical Federation, Paris, France, 2022.[6]Andreescu A M T, Crunteanu D E, Teodorescu M V, et al.Development and Testing of a Helicon Plasma Thruster Based on a Magnetically Enhanced Inductively Coupled Plasma Reactor Operating in a Multi-Mode Regime[J].Ap-plied Sciences, 2024, 14(18):8308-8308[7]Zheng P, Wu J, Zhang Y, et al.A Comprehensive Review of Atmosphere‐Breathing Electric Propulsion Systems[J].International Journal of Aerospace Engineering, 2020, 2020(1):8811847-8811847[8]孙安邦, 冯晨曦, 张思远, 等.超低轨道吸气式电推进技术研究进展与展望[J].航天 器环境工程, 2025, 42(3):239-255[9]SUN A B, FENG C X, ZHANG S Y, et al.Research progress and prospects of VLEO air-breathing electric propulsion[J].Spacecraft Environment Engineering, 2025, 42(3):239-255[10]Obrusník A, Bílek P, Hoder T, et al.Electric field deter-mination in air plasmas from intensity ratio of nitrogen spec-tral bands: ISensitivity analysis and uncertainty quantifica-tion of dominant processes[J].Plasma Sources Science and Technology, 2018, 27(8):085013-085013[11] Andreussi T, Cifali G, Giannetti V, et al.Development and experimental validation of a hall effect thruster ram-ep concept[C]//35th international electric propulsion conference, Atlanta, GA, USA, 2017.[12]Souhair N, Magarotto M, Andriulli R, et al.Prediction of the propulsive performance of an atmosphere-breathing elec-tric propulsion system on cathode-less plasma thruster[J].Aerospace, 2023, 10(2):100-100[13]任琼英, 葛丽丽, 郑慧奇, 等.超低轨吸气式螺旋波电推进概念研究[J].航天器环境工程, 2020, 37(01):17-24[14]REN Q Y, GE L L, ZHENG H Q, et al.The concept study of an air-breathing helicon thruster used in ultra-low orbit flight[J].Spacecraft Environment Engineering, 2020, 37(1):17-24[15]李永平, 朱光武, 郑晓亮, 等.超低轨道热层大气密度原位探测[J].北京航空航天大学学报, 2022, 48(10):1875-1882[16]LI Y P, ZHU G W, ZHENG X L, et al.In-situ measurement of atmospheric density in very low Earth orbits[J].Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(10):1875-1882[17] Hruby V, Hohman K, Szabo J.Air breathing hall effect thruster design studies and experiments[C]//37th Internation-al Electric Propulsion Conference, Boston, Massachusetts, IEPC-2022-446.[18]Andreussi T, Ferrato E, Kitaeva A, et al.Characteriza-tion of an atmospheric propellant-fed hall thruster as a vleo simulator[C]//37th International Electric Propulsion Confer-ence, Cambridge, USA. 2022.[19] 姜巍.射频容性耦合等离子体的两维隐格式PIC/MC模拟[D]. 大连理工大学, 2010.[20]JIANG W.Two-Dimensional Implicit PIC/MC Simulations for Radio-Frequency Capacitively Coupled Plasmas[D]. Dalian University of Technology, 2010.[21]ZHONG Y X, ZHANG Y, WU J J, et al.Optical detec-tion method of discharge mode transition of inductively cou-pled plasma in an atmosphere-breathing electric propulsion system[J].Chinese Journal of Aeronautics, 2024, 37(10):172-183[22]Takao Y, Ono K.A miniature electrothermal thruster using microwave-excited plasmas: a numerical design con-sideration[J].Plasma Sources Science and Technology, 2006, 15(2):211-227[23] Shinohara S.High-Density Helicon Plasma Science: From Basics to Applications[M]. Singapore: Springer Nature Singapore, 2022.[24]Ellingboe A R, Boswell R W.Capacitive,inductive and helicon‐wave modes of operation of a helicon plasma source[J].Physics of Plasmas, 1996, 3(7):2797-2804[25]Caneses J F, Blackwell B D.Collisional dam of helicon waves in a high density hydrogen linear plasma device[J].Plasma Sources Science and Technology, 2016, 25(5):055027-055027[26]Romano F, Chan Y A, Herdrich G, et al.RF Helicon-based Plasma Thruster (IPT): Design, Set-up, and First Ignition[C]//Space Propulsion Symposium. 2021.[27]Romano F, Chan Y A, Herdrich G, et al.RF helicon-based inductive plasma thruster (IPT) design for an atmos-phere-breathing electric propulsion system (ABEP)[J].Acta Astronautica, 2020, 176(2020):476-483[28] Masillo S, Romano F, Soglia R, et al.Analysis of elec-trodeless plasma source enhancement by an externally ap-plied magnetic field for an inductive plasma thruster (IPT)[C]//7th Russian-German Conference on Electric Pro-pulsion, Rauischholzhausen, Germany. 2018.[29]Romano F, Herdrich G, Chan Y A, et al.Design of an intake and a thruster for an atmosphere-breathing electric propulsion system[J].CEAS Space Journal, 2022, 14(4):707-715[30] Herdrich G, Skalden J, Behnke A, et al.An Overview of Recent Thrust Balance Developments at the Institute of Space Systems[C]//Conference Article: 37th International Electric Propulsion Conference, Massachusetts Institute of Technology, Cambridge, MA, USA. 2022.[31]Antipov S N, Sargsyan M A, Gadzhiev M Kh.Emission spectrum analysis of an atmospheric electrode microwave discharge in argon flow and of a cold plasma jet on its base[J].Journal of Physics: Conference Series, 2020, 1698(1):012029-012029[32]Chen F F.Langmuir probes in RF plasma: surprising validity of OML theory[J].Plasma Sources Science and Technology, 2009, 18(3):012029-012029[33]Chen F F.Langmuir probe measurements in the intense RF field of a helicon discharge[J].Plasma Sources Science and Technology, 2012, 21(5):055013-055013[34] 张天亮.螺旋波等离子体的模式转换和粒子动理学特性[D]. 北京理工大学, 2024.[35]ZHANG T L.Characteristics of mode transition and species kinetics in helicon plasmas[D]. Beijing Institute of Technol-ogy, 2024.[36]Zhu X M, Pu Y K.A simple collisional–radiative model for low-pressure argon discharges[J].Journal of Physics D: Applied Physics, 2007, 40(8):2533-2533[37]Czerwiec T, Graves D B.Mode transitions in low pres-sure rare gas cylindrical ICP discharge studied by optical emission spectroscopy[J].Journal of Physics D: Applied Physics, 2004, 37(20):2827-2827[38]Stewart R S, Smith D J.Complementary optical diag-nostic modelling of the argon positive column[J].Journal of Physics D: Applied Physics, 2002, 35(14):1777-1777[39]Loewenhardt P K, Blackwell B D, Boswell R W, et al.Plasma production in a toroidal heliac by helicon waves[J].Physical Review Letters, 1991, 67(20):2792-2794[40]Chen F F, Blackwell D D.Upper Limit to Landau Damping in Helicon Discharges[J].Physical Review Letters, 1999, 82(13):2677-2680[41]Molvik A W, Ellingboe A R, Rognlien T D.Hot-Electron Production and Wave Structure in a Helicon Plasma Source[J].Physical Review Letters, 1997, 79(2):233-236[42]Chen F F, Boswell R W.Helicons-the past decade[J].IEEE Transactions on Plasma Science, 1997, 25(6):1245-1257[43] 崔瑞林.氩气螺旋波等离子体的放电特性及波耦合机理[D]. 北京理工大学, 2022.[44]CUI R L.Discharge Characteristics and Wave Coupling Mechanism of Argon Helicon Plasma[D]. Beijing Institute of Technology, 2022.[45]Ding Z F, Yuan G Y, Gao W, et al.Effects of impedance matching network on the discharge mode transitions in a radio-frequency inductively coupled plasma[J].Physics of Plasmas, 2008, 15(6):063506-063506[46]Blackwell D D, Chen F F.Two-dimensional imaging of a helicon discharge[J].Plasma Sources Science and Technol-ogy, 1997, 6(4):569-576[47]Zhao G, Wang H, Si X, et al.The discharge characteris-tics in nitrogen helicon plasma[J].Physics of Plasmas, 2017, 24(12):123507-123507[48]Eom G S, Bae I D, Cho G, et al.Helicon plasma genera-tion at very high radio frequency[J].Plasma Sources Science and Technology, 2001, 10(3):417-417[49]Lafleur T, Charles C, Boswell R W.Characterization of a helicon plasma source in low diverging magnetic fields[J].Journal of Physics D: Applied Physics, 2011, 44(5):055202-055202 |
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