Millimeter Wave Doppler Radar Testing Using the Lunar Regolith Ejecta Simulator

Beverly W. Kemmerer; Austin R. Atkins; Daniel P. Batcheldor; Austin G. Langton; James G. Mantovani

NASA NTRS · 20230008210

Millimeter Wave Doppler Radar Testing Using the Lunar Regolith Ejecta Simulator

Beverly W. Kemmerer·Austin R. Atkins·Daniel P. Batcheldor·Austin G. Langton·James G. Mantovani

Abstract

A linear conveyor system has been devised to maintain lunar regolith simulant at a range of velocities, distances, angles, particle densities, and particle sizes. The Lunar Regolith Ejecta Simulator (LuRES) system shall test prototype and potential flight instrumentation for measuring the velocities of regolith particles accelerated by a plume-surface interaction (PSI) and determining effects of particle number densities and particle size distributions on return signals. Here we present the results of initial LuRES testing of the Millimeter Wave Doppler Radar (MWDR) instrument. The LuRES system held a single, ~900 µm BP-1 lunar regolith simulant particle at a continuous ~5 m/s velocity. The return signal of the MWDR from this LuRES configuration was analyzed to calibrate the MWDR instrument. Further testing is planned for the remaining of 2023 to calibrate the MWDR for various particle sizes and densities at a continuous velocity. These results will be presented in the final paper.

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BibTeX RIS

Beverly W. Kemmerer, Austin R. Atkins, Daniel P. Batcheldor, Austin G. Langton, James G. Mantovani. Millimeter Wave Doppler Radar Testing Using the Lunar Regolith Ejecta Simulator. https://ntrs.nasa.gov/citations/20230008210

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