Laser characterization of electric field oscillations in the Hall thruster breathing mode

ORAL

Abstract

Hall thrusters are a mature technology for space propulsion applications that exhibit a wide array of dynamic behavior, including plasma waves, instabilities and turbulence. One common low frequency (10--50 kHz) discharge current oscillation is the breathing mode, a cycle of neutral propellant injection, strong ionization, and ion acceleration by a steep potential gradient. A time-resolved laser-induced fluorescence diagnostic non-intrusively captures this propagating ionization front in the channel of a commercial BHT-600 Hall thruster manufactured by Busek Co. Measurements of ion velocity and relative ion density (using the $5d[4]_{7/2} - 6p[3]_{5/2}$ Xe II transition at 834.95 nm, vacuum) reveal a dynamic electric field structure traversing the channel throughout the breathing mode cycle.

Authors

  • Christopher Young

    Stanford University, Stanford Plasma Physics Laboratory

  • Andrea Lucca Fabris

    Stanford Plasma Physics Laboratory, University of Surrey

  • Natalia MacDonald-Tenenbaum

    Air Force Research Laboratory, Edwards AFB

  • William Hargus Jr.

    Air Force Research Laboratory, Edwards AFB

  • Mark Cappelli

    Stanford University, Stanford Plasma Physics Laboratory