Ultra-small satellite, onboard computer for CubeSat, CSP. A single-board computer equipped with a Zynq-7020 processor.
A low-power, high-performance onboard computer (CSP) for ultra-small satellites, CubeSats. This CSP is equipped with a microprocessor and FPGA, using the Xilinx Zynq-7020. It is also designed to be radiation-hardened for space use. Applications of the CSP include image processing, signal processing, and C&DH (Command and Data Handling), among others.
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basic information
The main specifications of the CSP are as follows: - Processor: Xilinx Zynq-7020 SOC with Dual-Core ARM Cortex A9 up to 667MHz - Programmable Logic: 85K logic cells - Memory: 4GB NAND Flash; 1GB DDR3 SDRAM - IO: 26x MIO (Multiplexed IO); EMIO: 24 differential pairs and 12 single-ended IO - Power Consumption: 1.6 to 3.6W - Operating Temperature Range: 0℃ to +70℃ - Radiation Resistance: TID 30 krads (100 krads option) - Weight: 82g - Dimensions: 8.81 x 8.95 x 1.73 cm
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Applications/Examples of results
We have a proven track record of using numerous ultra-small satellites, CubeSats, and others.
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The Advanced Technology Research Institute is an engineering company that supports space development and utilization, including rockets and artificial satellites, in Japan and around the world. We conduct a wide range of activities from the design and development of space systems, subsystems, and components for satellites and rockets, both small and large, to the sale of overseas space equipment. Additionally, we sell solar cells for space and ground use, and we design and develop solar cell panels for space as well as sell solar power generation modules and systems for ground use. For small satellites, including CubeSats, we provide system development from 1U to 12U, offer bus components, design and develop bus equipment, assemble satellites, and conduct integration and testing of satellites, including payloads. We also design, develop, and sell small electric propulsion systems for CubeSats and small satellites.