A project to design a test-bench for thermal and pressure conditions in which a CubeSat satellite is subjected in space.

Design and manufacture a mechanical testing bench for mechanical vibration of CubeSat satellites from 1U to 3U, according to NASA-GEVS standard: GSFC-STD-7000A.

A project to find a convenient mathematical model that allows to get the optimal mechanical design of a non-COTS reaction wheel for a 3U CubeSat attitude control.