I. Introduction
Since early 2000 CubeSat class is democratizing the space acess. This nanosatellite topology was created with the main goals the integration among researchers, students, professors and companies looking to low cost space mission; simplicity in the design; use of radio amateur frequency band and space qualification of the future small payloads [1] [2]. The standard size measures 10 cm each edge and weighs less than 1.3 kg, being called 1 unity (1U) [1]. Furthermore, launch costs are directly related to satellite mass and volume. So this topology have the opportunity to be launched into space orbit as a piggyback due to low mass and volume consequently minimizing launch costs.