• DocumentCode
    3115441
  • Title

    Effect of thruster scaling on pre-sheath and ion-loss region in Hall thrusters

  • Author

    Kawashima, R. ; Kaneko, R. ; Cho, Sangyeun ; Komurasaki, Kimiya ; Koizumi, Hirotaka ; Arakawa, Yasuhiko

  • Author_Institution
    Dept. of Aeronaut. & Astronaut., Univ. of Tokyo, Tokyo, Japan
  • fYear
    2012
  • fDate
    9-12 Oct. 2012
  • Firstpage
    513
  • Lastpage
    516
  • Abstract
    2-D plasma simulation of Hall thrusters based upon a hybrid particle-in-cell method has been conducted and the effect of thruster scaling on the ion-loss region and the degree of ions lost to the channel wall were investigated. The Bohm criterion was utilized for the boundary condition of the insulator wall and a magnetic field with plasma lens focusing was applied in the vicinity of the exit. The calculation results visualize the effects of pre-sheath and ion-loss region, which can be criteria for less-erosion designs. The results of thruster scaling show decreasing trends of the effects of ion-loss region and ion-loss fraction with increasing thruster size, which indicates that less erosion and better thrust efficiency are expected by thruster upsizing.
  • Keywords
    aerospace propulsion; magnetic fields; plasma focus; plasma sheaths; plasma simulation; 2D plasma simulation; Bohm criterion; Hall thrusters; boundary condition; channel wall; hybrid particle-in-cell method; insulator wall; ion-loss fraction; ion-loss region; magnetic field; plasma lens focusing; pre-sheath; thrust efficiency; thruster scaling; thruster size; thruster upsizing; Plasmas; Electric propulsion; Hall thruster; Hybrid particle-in-cell method; Plasma sheath;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Vehicle Power and Propulsion Conference (VPPC), 2012 IEEE
  • Conference_Location
    Seoul
  • Print_ISBN
    978-1-4673-0953-0
  • Type

    conf

  • DOI
    10.1109/VPPC.2012.6422748
  • Filename
    6422748