Published December 2005 | Version v1
Journal article

Plasma properties downstream of a low-power Hall thruster

  • 1. Air Force Research Laboratories, Edwards Air Force Base, Edwards, California 93524 (United States)
  • 2. Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, University of Michigan, College of Engineering, Ann Arbor, Michigan 48109 (United States)

Description

Triple Langmuir probes and emissive probes were used to measure the electron number density, electron temperature, and plasma potential downstream of a low-power Hall thruster. The results show a polytropic relation between electron temperature and electron number density throughout the sampled region. Over a large fraction of the plume, the plasma potential obeys the predictions of ambipolar expansion. Near the thruster centerline, however, observations show larger gradients of plasma potential than can be accounted for by this means. Radial profiles of plasma potential in the very-near-field plume are shown to contain large gradients that correspond in location to the boundaries of a visually intense plasma region

Additional details

Identifiers

Publishing Information

Journal Title
Physics of Plasmas
Journal Volume
12
Journal Issue
12
Journal Page Range
p. 123503-123503.8
ISSN
1070-664X
CODEN
PHPAEN

Optional Information

Notes
(c) 2005 American Institute of Physics