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Ground Slope Effects on Lander Radiator PerformanceTwo sensitivity studies were performed to examine the drop in radiator heat rejection from slopes. Study #1 used a 5.5m tall reduced order asset to represent a small-lander/rover. Study #2 used a 20m asset represent a tall lander. The assets had body mounted horizontal, 45º inward-tilted, and vertical radiator orientations. The impact of slopes on different radiator orientations and on radiators pointing different directions (i.e., slope verses sun) was investigated. The studies were conducted at a polar location of -82.5ºS to capture the incident solar flux at the northmost, and therefore the hottest, range of potential Artemis landing sites (Mons Mouton Plateau).
Document ID
20260002598
Acquisition Source
Johnson Space Center
Document Type
Presentation
Authors
Lisa Erickson ORCID
(Johnson Space Center Houston, United States)
Will Grier
(Langley Research Center Hampton, United States)
Will Birmingham
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
March 28, 2026
Publication Date
April 17, 2026
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Mechanical Engineering
Meeting Information
Meeting: Lunar Surface Slope Sensitivity Presentation
Location: Houston, TX
Country: US
Start Date: April 17, 2026
Sponsors: Johnson Space Center
Funding Number(s)
WBS: 954879.06.03.14.72
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
Keywords
Lunar Slope
Sensitivity Study
Heat Rejection
Sink Temperature
Radiator
Thermal Engineering
Lunar Surface
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