Achievements - Space

Onboard, Ground


Attitude and Orbital Control System (AOCS) for Microsatellites: Design and Development of Models and Software for the AOCS

Power Supply and Control Unit modules for space mission: RAMS Analysis (Reliability Analysis, FMECA, FTA) for several electronic boards

Interconnecting harness module: Reliability Analysis of onboard electromechanical device


EGSE (Electrical Ground Support Equipment): Development of software for command and monitoring of a CDE (Cooler Drive Electronic) system during integration and test phases

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