Paper 14145-211
Modular thermo-mechanical framework for agile prototyping of space instruments: the DUSTER case
7 July 2026 • 17:30 - 19:00 CEST | Hall B6
Abstract
The paper describes the thermo-mechanical framework developed for the DUSTER breadboard, aimed at integrating EMI-sensitive, high-voltage electronics in a configuration that remains practical for assembly and test. The enclosure is built from stacked aluminium frames supporting the DPU, the low- and high-voltage power supplies, and the sensor front-ends. Connector distribution was arranged to limit cable cross-routing and to keep kilovolt-level bias lines away from low-level analog paths. EMC control relies on conductive gaskets at the critical interfaces, while the thermal design follows a staged approach based on board-level conduction, internal heat links, and external baseplate coupling. This made it possible to introduce thermal improvements during laboratory testing without redesigning the enclosure.
Presenter
Instituto de Astrofisica de Andalucia - CSIC (Spain)
Mechanical and thermal engineer with over 20 years’ experience in scientific instrumentation for space and ground-based observatories. Track record includes the design and verification of electronic units for ESA missions (GIADA/Rosetta; PLATO Main Electronics Unit), optomechanical systems for radio astronomy (ALMA Band 1), and systems engineering for ground-based instrumentation (CARMENES, MARCOT). Recent work focuses on the mechanical–thermal architecture of DUSTER, an EU-funded multi-sensor instrument to study lunar dust. Presenting on behalf of the DUSTER Team.