First Cubesat Developed in Brazil

AESP-14 electrical block diagram

The electrical power subsystem was developed to supply electrical demand of AESP-14 system.

The onboard data handling was developed to store service and payload telemetry data during periods of time the satellite is not communicating with ground station.

The telemetry, tracking and command subsystem was developed to operate using the amateur radio UHF band.

The structural subsystem was designed to be as simply as possible, making the assembly and integration process easier.

After the development of all satellite subsystems, the system engineering is the area responsible of defining all the steps to be executed on the assembly and integration process.

As a payload and aplication for this nano satellite, was developed an amateur radio experiment.

Project team including systems engineering (undergraduate students) and development (master degree students) during the EMI test.

AESP14 team would like to thanks...