• DocumentCode
    1455810
  • Title

    Magnet Configuration and Experimental Analysis of Helicon Source for Space Magnetoplasma Propulsion

  • Author

    Wang, Yibai ; Li, Bo ; Zhang, Pizhuo ; Wang, Shouguo

  • Author_Institution
    Sch. of Astronaut., Beihang Univ., Beijing, China
  • Volume
    20
  • Issue
    3
  • fYear
    2010
  • fDate
    6/1/2010 12:00:00 AM
  • Firstpage
    993
  • Lastpage
    996
  • Abstract
    The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is one of the high performance electric propulsion devices for future interplanetary applications. Helicon sources can produce high-density plasmas with high-ionization efficiency suitable for VASIMR, which usually use two electromagnets to produce the required magnetic field configuration. How to optimal design the solenoids and how to create the requisite B-field are the key factors to affect the characteristics and performance of the helicon plasma. In this paper, the magnets were designed and fabricated, and an experimental helicon source was presented. Two solenoids situated around the cylindrical quartz tube were used to create an expanding magnetic field of about 250 G in the center decreasing to a few tens of Gauss in the downstream diffusion region. The antenna was powered by a radio-frequency (RF) system of 13.56 MHz, which maximum changeable power is 500 W. Our helicon device was installed with vacuum chamber that is pumped down to a base pressure of about 0.001 Pa using cryopumps. Langmuir probe is mounted on to measure the plasma parameters. It is found that, when increasing the radio-frequency power or varying the magnetic field, both the plasma density and operating mode of helicon-wave ion are also changed. Permanent magnets (PM) and High temperature superconducting (HTS) magnets are also considered to use in the helicon source, and relative analyses are discussed. The details of further research are to investigate the relationship that the applied magnets affect on the efficiency and performance of the helicon plasma.
  • Keywords
    Langmuir probes; aerospace propulsion; antennas in plasma; fusion reactor design; ionisation; plasma density; plasma devices; plasma magnetohydrodynamics; plasma pressure; plasma sources; superconducting magnets; Langmuir probe; VASIMR; cylindrical quartz tube; downstream diffusion region; electric propulsion device; experimental analysis; frequency 13.56 MHz; helicon device; helicon plasma; helicon source; helicon-wave ion; high temperature superconducting magnets; high-ionization efficiency; magnetic field configuration; maximum changeable power; plasma density; plasma operating mode; plasma parameter measurement; power 500 W; radio-frequency power; radio-frequency system; space magnetoplasma propulsion; vacuum chamber; variable specific impulse magnetoplasma rocket; Helicon; magnet; magnetoplasma; radio-frequency;
  • fLanguage
    English
  • Journal_Title
    Applied Superconductivity, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    1051-8223
  • Type

    jour

  • DOI
    10.1109/TASC.2010.2041443
  • Filename
    5439712