This article describes the design and elaboration of three test benches for CubeSats aerospace systems that, in view of the need for use and analysis of the constitutive subsystems, allow the characterization of variables such as position, acceleration, vibration, radiation, among other. These are, a gyroscope bench, an acceleration bench and a pneumatic bench. The gyroscope bench, designed for nanosatellite attitude control tests, is based on the assembly of two concentric hoops and a rotating base, which together allow 3 degrees of freedom. The Pneumatic bench is a compliment for the gyroscope bench, it allows attitude control test of a single axis. On the other hand, the acceleration bench consists of a DC motor coupled to a transmission arm and allows up to 5 acceleration gravities to be obtained; Its purpose is to evaluate the structural performance of aerospace systems and serve as a platform for accelerometer characterization. Each of the benches has a versatile clamping platform so that different types of small-scale systems such as nanosatellites and electronic devices can be tested. These tests seek to validate the operation and performance of the systems on board the satellite equipment, as well as project the use of banks to other types of aerospace systems such as rocket and / or rover systems, which can be provided from the academy and development research of the Colombian aerospace field.