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REPORT DATE (DD-MM-YYYY)
18-01-2007
REPORT TYPE
Journal Article
DATES COVERED (From -To)
TITLE AND SUBTITLE 5a. CONTRACT NUMBER
Laser-induced Fluorescence Measurements of Velocity within a Hall Discharge
ABSTRACTThe results of a study of laser-induced fluorescence velocimetry of neutral and singly ionized xenon in the plume and interior portions of the acceleration channel of a Hall thruster plasma discharge operating at powers ranging from 250 to 725 W are described. Axial ion and neutral velocity profiles for four discharge voltage conditions (100V, 160V, 200V, 250V) are measured as are radial ion velocity profiles in the near-field plume. Ion velocity measurements of axial velocity both inside and outside the thruster as well as radial velocity measurements outside the thruster are performed using laser-induced fluorescence with nonresonant signaldetection on the xenon ion 5d[4]7/2-6p[3]5/2 excitation transition while monitoring the signal from the 6s[2]3/2-6p[3]5/2 transition. Neutral axial velocity measurements are similarly performed in the interior of the Hall thruster using the 6s[3/2]02-6p[3/2]2 transition with resonance fluorescence collection. Optical access to the interior of the Hall thruster is provided by a 1-mm-wide axial slot in the insulator outer wall. While the majority of the ion velocity measurements used partially saturated fluorescence to improve the signal-to-noise ratio, one radial trace of the ion transition was taken in the linear fluorescence region and yields a xenon ion translational temperature between 400 and 800 K at a location 13 mm into the plume.