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A Data-Derived Scaling Approach for Plume-Surface Interaction Crater FormationThis work presents a methodology for scaling test-scale plume-surface interaction (PSI) crater formation data to flight-scale. Methods for scaling both crater erosion rate and crater geometry (width and depth) were derived from scaling relationships proposed by previous PSI studies. Two methods for predicting crater width were investigated - one using an empirical scaling law for the crater aspect ratio and another informed by surface shear stress profiles from computational fluid dynamics (CFD). Data from three independent studies were then used to assess the performance of the developed scaling methodology. Results show that data from all three sources agree well with the crater erosion rate scaling methodology, with the caveat that limited data exist in regimes truly relevant to landing on the Moon. The performance of the geometry scaling methodology was more nuanced. The empirical scaling for crater aspect ratio performed well against PSI data obtained under Earth-atmospheric ambient pressure, but did a poor job of predicting the aspect ratio of craters formed from highly underexpanded plumes under vacuum conditions. Data from the Human Landing System (HLS) program’s Plume Surface Interaction Ground Test will be used to further improve the performance of the scaling methodology and to provide flight-scale predictions for PSI effects caused by HLS landers.
Document ID
20250011216
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Daniel C Stubbs
(Marshall Space Flight Center Redstone Arsenal, United States)
Manish Mehta
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
December 9, 2025
Publication Date
January 12, 2026
Publication Information
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Lunar and Planetary Science and Exploration
Fluid Mechanics and Thermodynamics
Meeting Information
Meeting: AIAA SciTech Forum
Location: Orlando, FL
Country: US
Start Date: January 12, 2026
End Date: January 16, 2026
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 954879.04.02.62.14
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
plume
regolith
psi
plume surface interactions
plume-surface interactions
plume surface interaction
plume-surface interaction
landers
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