Power efficiency

EPS I

Flight-proven Electric Power System (EPS)

this cubesat module has flight heritage
this cubesat module is featured in NASA state of the art report
eps-1-cubesat-power-module-endurosat

Flight-proven Electric Power System (EPS)

2Xmore
efficient
ISScompliance
on demand
10.2Wh
capacity

2x lower power consumption than systems in the same class

eps-1-cubesat-power-module-endurosat

Power efficiency

Our EPS: 2x higher

INDUSTRY AVERAGE

Built-in redundant short-circuit and overvoltage protections

eps-1-cubesat-power-module-endurosat

Applications

science and research iconScience and Research
Education iconEducation
Technology demonstration iconTechnology Demonstration

Passive and active thermal management for optimal control of battery charging

eps-1-cubesat-power-module-endurosat

Features

Input Channels 3 (one for each CubeSat axis)
Input voltage (per Solar Panel Channel) up to 5.5 V
Input current (per Solar Panel Channel) up to 1.8 A
Six connectors for the solar panels
Integrated blocking diode for each solar panel connector
Battery pack power 10.2 Wh (20.4 Wh with EPS I Plus)
Battery pack voltage 3.7 V nominal
Mass 208 g
Stackable battery packs up to 8 A
Output power buses 3.3 V, 5 V, BCR (5 V max) and Battery raw
Interfaces UART, I2C, USB-C
Switches Two deployment and one Remove Before Flight (RBF)
Control Six general purpose outputs for shutdown/reset of external modules
Interfaces UART, I2C, USB

Compliant with the highest safety standards including ISS deployment on demand

eps-1-cubesat-power-module-endurosat

Included

user manual book icon Complete User Manual
included cables icon USB cable
customer support icon 5h engineering support
delivery cost icon Delivery cost
handling and administration costs icon Handling and administration costs