Influence of cusp-shaped magnetic fields on plasma density and thrust in an RF plasma thruster with a magnetic nozzle

被引:0
|
作者
Furukawa, Takeru [1 ]
Shimasaki, Kento [1 ]
Nakamoto, Satoshi [1 ]
Takeno, Hiromasa [1 ]
机构
[1] Kobe Univ, Kobe, Hyogo 6578501, Japan
基金
日本学术振兴会;
关键词
Compendex;
D O I
10.1063/5.0226228
中图分类号
O35 [流体力学]; O53 [等离子体物理学];
学科分类号
070204 ; 080103 ; 080704 ;
摘要
In a radiofrequency (RF) plasma thruster device utilizing a cusp-shaped magnetic field, we investigate the dependence of plasma parameters on operational conditions. Among the conditions, this study focused on the cusp-field condition and found that the axial profiles of the plasma parameters vary depending on the field conditions. The plasma density profile is affected by the distance between the cusp point and the position of the RF antenna. When the cusp strength increases, the cusp condition enhances plasma density and the total thrust, which is the sum of the thrust components of the electron static pressure and diamagnetic current. We propose an ideal cusp point concerning the antenna position for optimal performance in the thruster device. This paper highlights how cusp-shaped magnetic fields influence electron dynamics as an operational index of the RF plasma thruster with a magnetic nozzle.
引用
收藏
页数:8
相关论文
共 50 条
  • [21] Magnetic confinement in a ring-cusp ion thruster discharge plasma
    NASA Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Dr., Pasadena, CA 91109, United States
    J Appl Phys, 2009, 9
  • [22] Mechanism of heat and oxygen transfer under electromagnetic CZ crystal growth with cusp-shaped magnetic fields
    Kakimoto, K
    Tashiro, A
    Ishii, H
    Shinozaki, T
    JOURNAL OF THE ELECTROCHEMICAL SOCIETY, 2003, 150 (10) : G648 - G652
  • [23] Design of a Thrust Balance for RF Plasma Thruster Characterization
    Trezzolani, F.
    Romero, I. Pita
    Bosi, F.
    Melazzi, D.
    Pavarin, D.
    Manente, M.
    Selmo, A.
    2014 IEEE INTERNATIONAL WORKSHOP ON METROLOGY FOR AEROSPACE (METROAEROSPACE), 2014, : 462 - 467
  • [24] A HiPIMS plasma source with a magnetic nozzle that accelerates ions: application in a thruster
    Bathgate, Stephen N.
    Ganesan, Rajesh
    Bilek, Marcela M. M.
    McKenzie, David R.
    EUROPEAN PHYSICAL JOURNAL-APPLIED PHYSICS, 2016, 76 (03):
  • [25] Experimental identification of an azimuthal current in a magnetic nozzle of a radiofrequency plasma thruster
    Takahashi, Kazunori
    Chiba, Aiki
    Komuro, Atsushi
    Ando, Akira
    PLASMA SOURCES SCIENCE & TECHNOLOGY, 2016, 25 (05):
  • [26] Spatially- and vector-resolved momentum flux lost to a wall in a magnetic nozzle rf plasma thruster
    Takahashi, Kazunori
    Sugawara, Takeharu
    Ando, Akira
    SCIENTIFIC REPORTS, 2020, 10 (01)
  • [27] Spatially- and vector-resolved momentum flux lost to a wall in a magnetic nozzle rf plasma thruster
    Kazunori Takahashi
    Takeharu Sugawara
    Akira Ando
    Scientific Reports, 10
  • [28] Two-dimensional plasma-wave interaction in an helicon plasma thruster with magnetic nozzle
    Tian, Bin
    Merino, Mario
    Ahedo, Eduardo
    PLASMA SOURCES SCIENCE & TECHNOLOGY, 2018, 27 (11):
  • [29] Plasma Thruster Using Momentum Exchange in Crossed Magnetic Fields
    Karimov, Alexander R.
    Murad, Paul A.
    IEEE TRANSACTIONS ON PLASMA SCIENCE, 2018, 46 (04) : 882 - 887
  • [30] Density enhancement of an RF plasma in a magnetic quadrupole
    Teske, Christian
    Iberler, Marcus
    Jacoby, Joachim
    PLASMA SOURCES SCIENCE & TECHNOLOGY, 2008, 17 (02):