The STARBUCK-MINI from AAC Clyde Space is a PCDU (Power Conditioning and Distribution Unit) solution designed for SmallSat with a design life of 5-7 years in LEO orbit. It has a mass of 3.3 kg and a system power of 1500 W. This PCDU requires a primary bus voltage of 22–34 V and a secondary bus voltage of 5–15 V with an isolated ground. It offers advanced power management with Maximum Power Point Tracker/S3R and has optimized reliability with performance fail-safes. This ITAR-free PCDU can be controlled via CAN or RS422 interfaces. It measures 147 x 249 x 123 mm and is ideal for small satellites.
