Tesis

In the elaboration of satellite structures, materials called composites are mostly  used due to their excellent physical properties. These structures are called & quot; sandwich & quot;, they have a laminate of carbon fiber material called Facing and a core of aluminum material. These components are subjected to different tests, among which are the so-called & uot; qualification tests & quot; They correspond to a vibration analysis of the structure according to the requirements of the GEVS Standard (General Envarionmental Verifications Standard). It is carried out by means of an electrodynamic exciter called Shaker, where the frequency response of the system is obtained and it is subjected to vibrations. The following work aims to present the results obtained using the analysis techniques; of vibrations and extensometry, as an application of the Non-Destructive Testing Methods (NDT), in addition, a validation is presented through the finite element method, using the ANSYS V19.2 calculation code.