Computing and storage integrated architecture system

The invention relates to the technical field of spaceflight, and provides a calculation and storage integrated design architecture system, which comprises a processor system used for calculating and processing received load information and load data of an aircraft through a processor chip; the memory system is used for framing and storing load data and load information through a memory chip so as to realize read-write control and bad block management of a second memory chip; and the bridging system is used for connecting the processor system and the memory system to realize bidirectional interaction of the load information and the load data of the processor system and the load information and the load data between the memory systems. The weight of the whole aircraft can be effectively reduced, backup of memory system data with special requirements is achieved, and meanwhile the fusion operation capacity of the spacecraft system and the on-orbit reconstruction capacity of the processor system and the memory sy