Electrical Power System for CubeSats

SKU: C3S EPS-1000

Satellite Electrical Power System by C3S Electronics Development

Note : Your request will be directed to C3S Electronics Development.

C3S EPS-1000 Image

The C3S EPS-1000 from C3S Electronics Development is a Satellite Electrical Power System with a total input power of 46.9 W and an input current of 0.75 A. It has an output voltage of up to 12.6 V and an output surge voltage of 13.5 V. This radiation-tested EPS has a switching frequency of 400 - 480 kHz and an efficiency ranging from 65 - 89 %. It has up to 7 series triple junction solar cells and each solar cell has a programmable voltage range of 6 - 25 V. This flight-proven Micro-D main converter is compliant with MIL-DTL-83513 and features a Nano-D access port for battery charging and USB service interface. It supports redundant CAN bus for telemetry and telecommand communication. 

The EPS has a maximum of 50 W total incoming solar panel capacity. It comes with integrated overvoltage, overcurrent, overpower, configurable current limitation, and a two-level battery undervoltage protection. This ESA-qualified EPS has 3.3 V, 5 V, and unregulated voltage levels and is suitable for 3U/ 6U and 12U CubeSat platforms.

Product Specifications

Product Details

  • Part Number
    C3S EPS-1000
  • Manufacturer
    C3S Electronics Development
  • Description
    Electrical Power System for CubeSats

General Parameters

  • Space Heritage
  • Input Channel
    6 Channel
  • Input Current
    0.75 A
  • Input Voltage
    8 to 14 V
  • Mass
    811 g
  • Output Voltage
    3.3 to 5 V
  • Output Current
    4 A
  • Power Consumption
    46.9 W
  • Output Unregulated Bus Voltage
    9.9 to 12.3 V
  • Output Unregulated Bus Current
    5 A
  • Battery Pack Voltage
    8.4 V
  • Battery Pack Power
    50 Wh
  • Radiation
    10 Krad
  • Standard
  • Operating Temperature
    -40 to 80 Degree C
  • Dimension
    88.5 x 96 x 88.1 mm
  • Note

Technical Documents