In-situ Measurement of Erosion of Boron Nitride for Hall Thruster Lifetime Research
POSTER
Abstract
Hall Thrusters (HT) are a compelling choice for spacecraft propulsion due to their relatively high thrust-to-power ratio and high specific impulse [1]. Erosion of HT acceleration channel walls, made of ceramic material, by ionized propellant has a significant impact on HT lifetime [1-2]. To predict HT lifetime, experiments running the HT for thousands of hours under vacuum conditions are necessary. Measuring erosion as a function of the time during these tests necessitates either breaking vacuum repeatedly and using ex-situ methods or implementing an in-situ erosion measurement system. This work describes the preliminary testing of a long-distance microscope (LDM) and Shape-From-Focus approach [3] to measure erosion of a Boron Nitride (BN) surface under conditions similar to those in the HT acceleration channel. Tests were conducted with a Maksutov-Cassegrain type LDM mounted on a motorized stage. The BN surface was modified to accelerate the erosion process to speed up testing. Optimal sample geometry was determined based on a semi-empirical sputtering model [4].
Publication: [1] J. Simmonds, Y. Raitses, and A. Smolyakov, J. Electric Propulsion 2, 12 (2023).<br>[2] N. Brown and M. Walker, Appl. Sci 10, 3775 (2020).<br>[3] A. Ottaviano et al., Rev. Sci. Instrum. 92, 073701 (2021).<br>[4] Y. Yamamura and H. Tawara, Atomic Data and Nuclear Tables 62, 149 (1996).
Presenters
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Jacob A Kiviat
Cornell University
Authors
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Jacob A Kiviat
Cornell University
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Ishaan Mishra
Rose-Hulman Institute of Technology
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Ivan Romadanov
Princeton Plasma Physics Laboratory
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Yevgeny Raitses
US Dept of Energy-Germantown, Princeton Plasma Physics Laboratory, Princeton Plasma Physics Laboratory, Princeton, NJ 08540, Princeton Plasma Physics Laboratory, Princeton University