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Advanced avionics and data processing

EPS I PLUS

Power Efficiency + Capacity
Cad file & datasheet
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Cad file & datasheet
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2X
MORE EFFICIENT
50+
YEARS OF FLIGHT HERITAGE
20.4
WH CAPACITY

Flight-proven Electric Power System (EPS)

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
Integrated Blocking Diode
for each solar panel connector
Battery Pack Power
20.4 Wh (10.2 Wh with EPS I)
Battery Pack Voltage
3.7 V nominal
Mass
330 g
Stackable Battery Packs
up to 8 A
Output Power Buses
3.3 V, 5 V, BCR (5 V max) and Battery raw
Interfaces
RS-485, USB-C
Switches
Two deployment and one Remove Before Flight (RBF)
Control
Six general purpose outputs for shutdown/reset of external modules
EPS I Plus web render 5
Power Efficiency + Capacity

Included

Complete User Manual
USB cable
5h engineering support
Delivery cost
Handling and administration costs
Flight-proven Electric Power System (EPS)
EPS I Plus 3
EPS I Plus web render 4

2x lower power consumption than systems in the same class

EPS I Plus web render 1

Built-in redundant short-circuit & overvoltage protections

EPS I Plus web render 3

Passive & active thermal management for optimal control of battery charging

EPS I Plus web render 2

Over fifty years of flight heritage

200% BIGGER BATTERY CAPACITY THAN EPS I AT 40% LARGER VOLUME
Related Products
EPS I
EPS I
Battery Pack Power
10.2 Wh
Battery Pack Voltage
3.7 V nominal
Mass
230 g
EPS IIbat
EPS II + Battery Pack
Processor
ARM Cortex M7
Program Memory Size
2 MB
SRAM
1 MB
2500
MODULES IN ORBIT
50
DELIVERED SATELLITES
200
TB DATA DOWNLINKED
All our products undergo Space Qualification, involving stringent testing under extreme conditions to ensure their robustness and high performance
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