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To lower the total weight of the rover while keeping its high mechanical properties using hybrid fabrication processes.

To decrease the heat losses of the rover structure, preventing the internal electronics from reaching destructive cold temperatures during lunar nights.

Keywords : Aerospace – Lunar Rover – FDM – Advanced composites – PEEK and PEEK-based composites – Heat transfer – Sandwich panels – Honeycomb structures – Improvement of the mechanical properties – Weight stabilization.

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