Small satellite is the integration of light weight, small volume and low launch cost. It is a promising approach to realize
the future space mission. A detailed study of the data management system has been carried out, with using new
reconfiguration method based on System On Programmable Chip (SOPC). Compared with common structure of satellite,
the Central Terminal Unit (CTU), the Remote Terminal Unit (RTU) and Serial Data Bus (SDB) of the data management
are all integrated in single chip. Thus the reliability of the satellite is greatly improved. At the same time, the data
management system has powerful performance owing to the modern FPGA processing ability.
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