Electrical Power Subsystem (EPS)



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It is the SubSystem that performs:

The EPS includes the following units: Energy storage (465 Wh) and its delivery to the Satellite users during the Eclipse period (37 min) is performed by a battery system consisting of two NiCd battery of 36 cells each with a name plate capacity of 30 Ah.

Withstanding of the 13000 charge/discharge cycles required by the SAX minimum operative life is ensured by limiting the battery Depth Of Discharge (DOD) to 25%.

The PCU performs the regulation of the power bus voltage (29 V nominal) during the sunlight period through shunt regulators for each solar panel main section power line.

The BCDR controls the battery charge/discharge by means of:

The PPDU provides the power distribution by splitting the different output lines to the end users and ensures protection against overcurrent by electronic current limiters.

The BCU performs battery status monitoring (voltage and temperature) and takes automatic protective actions mainly consisting of:


This file was last modified on Wednesday, 02-Sep-1998 17:28:57 CEST by Mauro Orlandini


next previous up Contents
Next: Solar Array (SAS) Previous: Reaction Control (RCS)
Up: SAX Home Page Contents: Table of Contents