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NASA Plume-Surface Interaction (PSI) Testing to Reduce Risk from Propulsive LandingNASA's Artemis program will return humans to the surface of the Moon for the first time since the final Apollo mission in December 1972. The new lunar landers are larger, more powerful, and utilize different concepts of operations from those flown during the Apollo era. During descent and landing, the environment resulting from the impingement of rocket engine exhaust onto regolith, or plume-surface interactions (PSI), poses a potential hazard to all propulsive landing vehicles, as well as nearby assets and payloads supporting exploration of the surface. Understanding these phenomena has challenged lander design since the 1960s, and new test data are required to enable NASA’s lunar exploration goals and to safely fly these new vehicles. At present, NASA is conducting ground testing in a vacuum sphere to obtain data relevant for prediction of the PSI environments produced by human-scale landing systems. This presentation will discuss the test objectives, design, execution, challenges, and data products.
Document ID
20260004959
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Ashley M Korzun
(Langley Research Center Hampton, United States)
Casey J Broslawski
(Langley Research Center Hampton, United States)
Wesley A Chambers
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
June 1, 2026
Subject Category
Aircraft Design, Testing and Performance
Meeting Information
Meeting: International Planetary Probe Workshop (IPPW-2026)
Location: Washington, D.C.
Country: US
Start Date: June 22, 2026
End Date: June 26, 2026
Sponsors: Johns Hopkins University Applied Physics Laboratory
Funding Number(s)
WBS: 954879.04.02.23.15
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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