The NANOeps subsystem consists of a power control & distribution module coupled with a battery management module, featuring a scalable integrated battery pack (up to 172 Wh). This makes it one of the most advanced EPS available for nano and microsatellites platforms. The NANOeps includes active balancing to ensure exceptional lifespan and heating system for optimal protection of each battery cell. It is capable of supplying power through 23 independent channels, three of which are redundant. Additionally, the system features five dedicated deployment actuator interfaces, separation and remove before flight switches, and many other functionalities. The comprehensive subsystem’s TM (currents, voltages, temperatures, etc.) and TC is provided over cold redundant CAN interface. The NANOeps is fully complaint with up to two NANOeps-AMPPT subsystems. KEY FEATURES • Battery Management Module (BMM) and battery pack • Battery capacity of 172Wh • Battery lifetime more then 30000 re-charge cycles @ 20% DoD (>80% EOL capacity) - 3 years in LEO • Superior thermal and chemical stability of LiFePO4 , stable under overcharge or short circuit • No capacity lost, due to low temperature conditions • High efficiency Inductive Couple Battery Balancer • Integrated Autonomous Battery Heaters per each battery cell • Individually Monitored and Controlled Power Distribution Power Control and Distribution Unit (PCDU) • 5x redundant DA interfaces with redundant TLM inputs • 3x separation switches • Provided up to 23 dedicated LCL protected output channels -3V3, 5V, 12V and Unregulated -Redundant architecture for essential outputs -Each output channel is adjustable with current up to 5 Amps Design • SEE immune design • Fault-tolerant SoC design • LUT-based supervisor • Instant boot up at power on • Redundant CAN interface for TM/TC • Fully autonomous satellite diagnostic data acquisition system • Debug connector for monitoring output channels and battery voltage during integration