Thermal Interaction of Mobile Ground Systems with Boulders on the Lunar Surface

The paper at hand evaluates the necessity of depicting topographic features like boulders on the lunar environment in thermal analyses for a size of up to 6.5 m in diameter. The question regarding the thermal influence becomes relevant when analysing a technical system within the lunar environment. This influence on the thermal behaviour of a test object is investigated in sensitivity studies. It is shown that the local surroundings can significantly alter a system’s net heat flux and can lead to overheating or critically cooling down instead of theoretically surviving when not considering local topographic features. Especially for small and lightweight systems ≤20 kg, like micro rovers, the effect of the surrounding on the system’s temperature becomes critical due to the low thermal capacity. Thus, it is a substantial aspect to be accounted for during the design phase as well as in mission operation.

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Publication Details

Published
2025-03-13
DOI
https://doi.org/10.3390/engproc2025090035
Primary Topic
Planetary Science and Exploration
Type
article
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article

Thermal Interaction of Mobile Ground Systems with Boulders on the Lunar Surface

Philipp Reiss, Markus Czupalla, Joel Guetzlaff
Planetary Science and Exploration
article

Thermal Interaction of Mobile Ground Systems with Boulders on the Lunar Surface

Philipp Reiss, Markus Czupalla, Joel Guetzlaff
article en

Abstract

The paper at hand evaluates the necessity of depicting topographic features like boulders on the lunar environment in thermal analyses for a size of up to 6.5 m in diameter. The question regarding the thermal influence becomes relevant when analysing a technical system within the lunar environment. This influence on the thermal behaviour of a test object is investigated in sensitivity studies. It is shown that the local surroundings can significantly alter a system’s net heat flux and can lead to overheating or critically cooling down instead of theoretically surviving when not considering local topographic features. Especially for small and lightweight systems ≤20 kg, like micro rovers, the effect of the surrounding on the system’s temperature becomes critical due to the low thermal capacity. Thus, it is a substantial aspect to be accounted for during the design phase as well as in mission operation.

Technical University of Munich (DE), FH Aachen (DE)
Openalex Percentile: Top 96%
Planetary Science and Exploration
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