Full EPS delivery based on mission requirements. Completely customized battery power delivery system designed uniquely on requirements provided by the customer.
High customization in terms of power and capacity
– In-house developed battery made of individual cell modules
– Each battery rigorously mechanically and electrically tested before flight
– Maximum reliability ensured via high QC standards
– Communication bus available to provide battery status to the spacecraft
– Ability to automatically reboot whole spacecraft in case the spacecraft stops responding
– Advanced self monitoring features built in to ensure reliable and safe operation of the battery and power delivery monitoring
– Solar charging including MPPT for best charging performance
– Power mass ratio 130-200 Wh/kg
– Voltage, current, temperature telemetry (over CAN or RS422)
– Flight heritage + 30 satellites
Single Module specifications | Missions | ||
Cells | 8x 18650 Li-ion (LG MJ1) | APEX – Commercial and Space force missions | |
Mass | 480 g | ReOrbit – UKKO | |
Rated capacity | 3.5 Ah | Reflex – SIGI | |
Nominal Output Voltage | 28 V | NASA – Mars Stationary Orbiter | |
Output Current | 8 A | ICEYE – SAR constellation | |
Nominal Input Voltage | 40 V | ESA – Perla – new type of Battery and PDU system | |
Input Current | 1.75 - 3.5 A | Development for ESA FLPP | |
