NASA NTRS · 20220013110
Regolith Simulant Preparation and Geotechnical Characterization for Plume Surface Interaction Testing
Abstract
Descent engine plumes interact with the lunar surface and accelerate regolith particles to potentially high velocities. These ejecta create risks to surface assets that have yet to be fully assessed. To better understand these risks, plume surface interactions can be simulated on the ground by firing a test engine plume into a bin of lunar regolith simulant under vacuum conditions. The dynamics of the resultant ejecta can then be recorded. In this technical memorandum we discuss the processes used in preparing a 150 kg bin of lunar regolith simulant for plume surface interaction ground tests under vacuum conditions for the NASA STMD Plume Surface Interaction project. We present our approach to mitigating regolith simulant eruptions during pump-down, the methods used to fill and reset the regolith simulant bin for each test, and the techniques used to characterize the consistency of regolith simulant geotechnical properties before each new firing. The challenges of preparing a regolith simulant test bin below an ambient pressure of one atmosphere, particularly on the large scale, could largely be overcome with a system that could fill the test bin with simulant inside the chamber and under vacuum conditions.
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James Mantovani, Austin Langton, Beverly Kemmerer, Austin Atkins, Daniel Batcheldor. 2022-09-09. Regolith Simulant Preparation and Geotechnical Characterization for Plume Surface Interaction Testing. https://ntrs.nasa.gov/citations/20220013110
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