The Micro satellite power system comprises a shunt regulating unit, filtered power supply unit, and autonomous charging circuit. Through charge and discharge adjustment and control of solar panels and battery packs, the primary power supply transformation control of the electrical power system is completed to meet the demand for electrical power supply of payloads and subsystems of the satellite. Meanwhile, the power system's telemetry data and control parameters are generated. The Microsatellite power system has light mass, small size, and high power density.

Power:100W~1500W;

Shunt regulating unit, filtered power supply unit. Telemetry and Telecommand unit, etc.;

Operating temperature: -20°C~60°C;

Structure: aluminum, black anodized;

Suitable for satellites over 20kg.