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We present the initial results from a cavity ring-down sensor for measuring the density of sputtered boron atoms originating from the discharge channel of a 6-kW Hall thruster. The sensor traps 250 nm light in a high-finesse cavity to greatly increase its sensitivity to boron atoms. Measurements were obtained with the thruster operating at seven conditions spanning discharge voltages from 150 to 600 V, and anode mass flow rates from 10 to 30 mg/s. Power level at these operating conditions ranged from 1.5 to 10 kW. Boron density was found to vary from <1×10 14 to ~1×10 15 m -3 with the higher density measurements being found near the two channel walls. We apply a simple two-dimensional velocity model to obtain boron flux. The boron flux is then correlated to the boron nitride sputter rate, which is found to vary from 4×10 -4 to 6×10 -3 mm 3 /s. A simple power law equation is formulated to correlate the relative sputter rate for the 6-kW Hall thruster as a function of the tested operating conditions. Although the uncertainty in this initial result is high, the result clearly demonstrates previously untapped potential for the use of cavity ring-down spectroscopy to study the problem of Hall thruster channel wall erosion.

Initial Cavity Ring-Down Density Measurement on a 6-kW Hall Thruster