Xenon tracers for cost effective laser induced fluorescence of alternative propellant Hall thrusters

Author:

Simmonds J. B.1ORCID,Byrne M. P.1ORCID,Chaplin V. H.1ORCID

Affiliation:

1. Jet Propulsion Laboratory, California Institute of Technology , Pasadena, California 91011, USA

Abstract

One of the limiting factors to developing plasma thrusters on alternative propellants is the cost associated with changing the diagnostic tools, which are often propellant-dependent. For laser induced fluorescence (LIF), which is typically used for ion velocity distribution measurements to determine ion trajectories and potential profiles, either new lasers need to be bought, which are tuned to the wavelength of the new element’s excitation level, or a costly tunable laser is required. A method to use existing LIF setups designed for xenon on any propellant has been demonstrated on a Hall thruster operating on krypton. In the demonstration test, a small amount of xenon (0.01%–4%) was mixed with the main krypton propellant for use as a diagnostic tracer, and xenon ion velocities were measured while also monitoring changes in the mean discharge current and oscillations. High signal-to-noise ratios in LIF data acquired along the channel centerline were obtained with tracer gas fractions ≤1% that negligibly affected the thruster operation. These results and comparison of the emission spectra of xenon and other common propellants suggest that the tracer LIF method should be broadly applicable to LIF measurements in Hall thrusters operating on alternative propellants.

Funder

National Aeronautics and Space Administration

Publisher

AIP Publishing

Reference26 articles.

1. Efficiency analysis of a Hall thruster operating with krypton and xenon;J. Propul. Power,2006

2. Investigation into the efficiency gap between krypton and xenon operation on a magnetically shielded Hall thruster

3. Performance comparison of a 9-kW magnetically shielded Hall thruster operating on xenon and krypton;J. Appl. Phys.,2021

4. Laser-induced fluorescence study of a xenon Hall thruster;Appl. Phys. B: Lasers Opt.,1997

5. Perturbations induced by electrostatic probe in the discharge of Hall thrusters;Rev. Sci. Instrum.,2016

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