This work presents the thermo-mechanical design of LD GRIDS (Lunar Dust GRID System), a dust analyser developed for the characterisation of the lunar environment. Starting from previous feasibility studies, which assessed the feasibility of the development of the sensing elements (i.e. sensing grids), the design is refined, defining the mechanical structure for hosting the sensing elements, with particular attention to thermal loads, mechanical integrity, and dynamic behaviour. A design solution able to provide required compliance for the in-plane thermal deformations while preserving out-of-plane stiffness and alignment of the sensing grids was detailed. The design is evaluated through a comprehensive numerical campaign including sensitivity, modal, quasi-static, thermo-elastic, and random vibration analyses. Results showed that the selected configuration satisfies dynamic requirements, maintaining stress state within acceptable limits under the simulated loading conditions, and meets applicable safety margins. A mock-up was manufactured to validate the developed design, supporting future experimental validation preliminarily. The experimental outcomes confirm the suitability of the proposed design for further experimental assessment, mainly focusing on qualification and functionality assessment in a representative environment.

Lunar Dust GRID System: Thermomechanical Study of a Charged Dust Analyser for the Lunar Surface

Ahmed A. M. R. M.;Scaccabarozzi D.;Izzo F.;Martina C.;Appiani A.;Potemkin K.;Corti M. G.;Saggin B.;
2026-01-01

Abstract

This work presents the thermo-mechanical design of LD GRIDS (Lunar Dust GRID System), a dust analyser developed for the characterisation of the lunar environment. Starting from previous feasibility studies, which assessed the feasibility of the development of the sensing elements (i.e. sensing grids), the design is refined, defining the mechanical structure for hosting the sensing elements, with particular attention to thermal loads, mechanical integrity, and dynamic behaviour. A design solution able to provide required compliance for the in-plane thermal deformations while preserving out-of-plane stiffness and alignment of the sensing grids was detailed. The design is evaluated through a comprehensive numerical campaign including sensitivity, modal, quasi-static, thermo-elastic, and random vibration analyses. Results showed that the selected configuration satisfies dynamic requirements, maintaining stress state within acceptable limits under the simulated loading conditions, and meets applicable safety margins. A mock-up was manufactured to validate the developed design, supporting future experimental validation preliminarily. The experimental outcomes confirm the suitability of the proposed design for further experimental assessment, mainly focusing on qualification and functionality assessment in a representative environment.
2026
Conference Proceedings - 2026 IEEE 13th International Workshop on Metrology for AeroSpace, MetroAeroSpace 2026
charged dust particles analyser
EMM project
LD GRIDS
Lunar surface
thermo-mechanical design
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/1325552
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