Remote Segment

Instruments

To be written...

Platform

To be written...

Power System

The Electrical Power System (EPS) ...

PCDU

The Power Conditioning and Distribution Unit (PCDU) is in charge of processing all the electrical power needed for operation of the spacecraft. It comprises the following main functions: - Condition the power coming from solar panels and batteries - Manage and monitor the battery state of charge - Distribute power within the spacecraft via protected and regulates lines - Connect/disconnect battery - Provide interface for telecommands and telemetry

Ground Support Equipment

To be written...