Progress on the research of helicon plasma thruster

被引:0
|
作者
Xia, Guang-Qing [1 ]
Wang, Dong-Xue [2 ]
Xue, Wei-Hua [3 ]
Zhang, Jia-Liang [1 ,2 ]
机构
[1] State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, China
[2] School of Physics and Optoelectronic Engineering, Dalian University of Technology, Dalian 116024, China
[3] Faculty of Electronic Information and Electrical Engineering, Dalian University of Technology, Dalian 116024, China
来源
关键词
33;
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
页码:857 / 863
相关论文
共 50 条
  • [41] Progress in the Development of a High Power Helicon Plasma Source for the Materials Plasma Exposure Experiment
    Goulding, R. H.
    Caughman, J. B. O.
    Rapp, J.
    Biewer, T. M.
    Bigelow, T. S.
    Campbell, I. H.
    Caneses, J. F.
    Donovan, D.
    Kafle, N.
    Martin, E. H.
    Ray, H. B.
    Shaw, G. C.
    Showers, M. A.
    FUSION SCIENCE AND TECHNOLOGY, 2017, 72 (04) : 588 - 594
  • [42] Development of a helium collisional radiative model for a helicon thruster
    Faust A.J.
    Sedwick R.J.
    Plasma Research Express, 2019, 1 (02):
  • [43] Ion production cost of a gridded helicon ion thruster
    Williams, Logan T.
    Walker, Mitchell L. R.
    PLASMA SOURCES SCIENCE & TECHNOLOGY, 2013, 22 (05):
  • [44] Low-pressure, high-density, and supersonic plasma flow generated by a helicon magnetoplasmadynamic thruster
    Takahashi, Kazunori
    Komuro, Atsushi
    Ando, Akira
    APPLIED PHYSICS LETTERS, 2014, 105 (19)
  • [45] Laser-induced fluorescence spectroscopy on xenon atoms and ions in the magnetic nozzle of a helicon plasma thruster
    Vinci, Alfio E.
    Mazouffre, Stephane
    Gomez, Victor
    Fajardo, Pablo
    Navarro-Cavalle, Jaume
    PLASMA SOURCES SCIENCE & TECHNOLOGY, 2022, 31 (09):
  • [46] Increased Thrust-to-Power Ratio of a Stepped-Diameter Helicon Plasma Thruster with Krypton Propellant
    Takahashi, Kazunori
    Takao, Yoshinori
    Ando, Akira
    JOURNAL OF PROPULSION AND POWER, 2020, 36 (06) : 961 - 965
  • [47] System design study of a VLEO satellite platform using the IRS RF helicon-based plasma thruster
    Herdrich, G.
    Papavramidis, K.
    Maier, P.
    Skalden, J.
    Hild, F.
    Beyer, J.
    Pfeiffer, M.
    Fugmann, M.
    Klinker, S.
    Fasoulas, S.
    Souhair, N.
    Ponti, F.
    Walther, M.
    Wiegand, A.
    Walpot, L.
    Duesmann, B.
    Borras, E. B.
    Roberts, P. C. E.
    Crisp, N. H.
    ACTA ASTRONAUTICA, 2024, 215 : 245 - 259
  • [48] Experimental investigation of a conical helicon double layer thruster arrangement
    Charles, C.
    Cox, W.
    Boswell, R. W.
    Laine, R.
    Perren, M.
    PLASMA SOURCES SCIENCE & TECHNOLOGY, 2010, 19 (04):
  • [49] An experimental investigation of alternative propellants for the helicon double layer thruster
    Charles, C.
    Boswell, R. W.
    Laine, R.
    MacLellan, P.
    JOURNAL OF PHYSICS D-APPLIED PHYSICS, 2008, 41 (17)
  • [50] Operating the helicon double layer thruster in a space simulation chamber
    Charles, Christine
    Boswell, Rod
    Alexander, Peter
    Costa, Costanzo
    Sutherland, Orson
    Pfitzner, Leigh
    Franzen, Roger
    Kingwell, Jeff
    Parfitt, Andrew
    Frigot, Pierre-Etienne
    Del Amo, Jose
    Saccoccia, Georgio
    IEEE TRANSACTIONS ON PLASMA SCIENCE, 2008, 36 (04) : 1196 - 1197