EPS I - Power Module - EnduroSat - Orbital Transports
Additional Information
Input Voltage:
up to 5.5 V per channel
Input Current:
up to 1.8 A per channel
Number of Channels:
3
Battery Power:
10.2 Wh
Battery Voltage:
3.7 V nominal
Power Consumption:
20 mA @3.7 V
Power Output:
3.3 V
Power Output:
5 V
Power Output:
BCR (5 V max)
Interface:
UART
Interface:
I2C
Interface:
USB
Mass:
208 g
Documentation

The EnduroSat CubeSat Electric Power System (EPS I) has the highest power efficiency in its class. It supports a wide range of outputs making it a versatile solution fully compliant with the CubeSat standard. Our CubeSat EPS module has flight heritage, including the ISS-level requirements.

Features:

  • Three Solar Panel Channels (one for each CubeSat axis: x, y and z)
  • Six connectors for the solar panels
  • Integrated blocking diode for each solar panel connector
  • Stackable battery packs up to 8A
  • Two deployment and one Remove Before Flight (RBF) switches can be connected
  • Six general purpose outputs for shutdown/reset of external modules
  • Latch-up protected 3.3V and 5V outputs

Includes:

  • USB debug & battery charger
  • Packed in a custom box
  • 5 hours of engineering support
  • Full warranty
  • Technical information (Datasheet)

Qualification:

Space qualification tests are performed on the Qualification Engineering Model. Qualification test levels and duration will follow the ESA standard ECSS-E-ST-10-03C and GEVS: GSFC-STD-7000A.

CubeSat EPS I Power Module

EnduroSat
Description

The EnduroSat CubeSat Electric Power System (EPS I) has the highest power efficiency in its class. It supports a wide range of outputs making it a versatile solution fully compliant with the CubeSat standard. Our CubeSat EPS module has flight heritage, including the ISS-level requirements.

Features:

  • Three Solar Panel Channels (one for each CubeSat axis: x, y and z)
  • Six connectors for the solar panels
  • Integrated blocking diode for each solar panel connector
  • Stackable battery packs up to 8A
  • Two deployment and one Remove Before Flight (RBF) switches can be connected
  • Six general purpose outputs for shutdown/reset of external modules
  • Latch-up protected 3.3V and 5V outputs

Includes:

  • USB debug & battery charger
  • Packed in a custom box
  • 5 hours of engineering support
  • Full warranty
  • Technical information (Datasheet)

Qualification:

Space qualification tests are performed on the Qualification Engineering Model. Qualification test levels and duration will follow the ESA standard ECSS-E-ST-10-03C and GEVS: GSFC-STD-7000A.

Current Stock:
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Additional Information
Input Voltage:
up to 5.5 V per channel
Input Current:
up to 1.8 A per channel
Number of Channels:
3
Battery Power:
10.2 Wh
Battery Voltage:
3.7 V nominal
Power Consumption:
20 mA @3.7 V
Power Output:
3.3 V
Power Output:
5 V
Power Output:
BCR (5 V max)
Interface:
UART
Interface:
I2C
Interface:
USB
Mass:
208 g
Documentation

The EnduroSat CubeSat Electric Power System (EPS I) has the highest power efficiency in its class. It supports a wide range of outputs making it a versatile solution fully compliant with the CubeSat standard. Our CubeSat EPS module has flight heritage, including the ISS-level requirements.

Features:

  • Three Solar Panel Channels (one for each CubeSat axis: x, y and z)
  • Six connectors for the solar panels
  • Integrated blocking diode for each solar panel connector
  • Stackable battery packs up to 8A
  • Two deployment and one Remove Before Flight (RBF) switches can be connected
  • Six general purpose outputs for shutdown/reset of external modules
  • Latch-up protected 3.3V and 5V outputs

Includes:

  • USB debug & battery charger
  • Packed in a custom box
  • 5 hours of engineering support
  • Full warranty
  • Technical information (Datasheet)

Qualification:

Space qualification tests are performed on the Qualification Engineering Model. Qualification test levels and duration will follow the ESA standard ECSS-E-ST-10-03C and GEVS: GSFC-STD-7000A.