Satellite electrical power system (EPS)

Products and reference designs

Satellite electrical power system (EPS)

Block diagram

Overview

Satellites harness power from solar panels to power spacecrafts. This high voltage supply needs to be stored and converted for all the onboard electronics. Our large portfolio of space-qualified devices and reference designs help you maximize your system performance.

Design requirements:

Modern satellite electrical power systems (EPS) require:

  • Multiple low noise and efficient point-of-load supplies.
  • Efficient isolated power supplies to convert the main bus to point-of-load supplies.
  • A feedback method to monitor the secondary supply rail.

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Block diagram

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Technical documentation

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Type Title Date
Selection guide TI Space Products (Rev. I) 10 Nov 2022
E-book Radiation Handbook for Electronics (Rev. A) 28 Oct 2020
Application note Failure Containment in Spacecraft Point-of-Load Power Supplies 30 Apr 2020
Application note Measuring Die Temperature with Remote Diode Sensing in Space 13 Dec 2018
Application note Use of an LDO as a Load Switch for Space Applications 01 Aug 2018
Application note TI Space Rated Power Solution for Microsemi® RTG4™ FPGA (Rev. A) 27 Jul 2018

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