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Spacecraft Systems In Production

SoC2016 32-bit Space Application On-Chip System

The SoC2016 is the first domestically developed heterogeneous multi-core SoC designed for integrated satellite control and data processing applications. It combines a Cortex-A9 processor core with a DSP digital signal processor, floating-point processor, and multiple communication interfaces including 1553B, CAN, and SpaceWire buses, as well as a DMA controller. The chip achieves performance exceeding 1000 MIPS @ 500 MHz, with power consumption below 3 W, reaching advanced international standards.

SoC2016 32-bit Space Application On-Chip System

Key Specifications

Process Technology
0.13 μm
Dimensions (mm)
41 × 41 × 10
Weight (g)
12
Operating Temperature (°C)
−55 to +125
Storage Temperature (°C)
−65 to +150
Communication Interface
SpaceWire / 1553B / CAN / RS-422
Published: October 16, 2025 Last updated: November 21, 2025
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Quick Overview

The SoC2016 is the first domestically developed heterogeneous multi-core SoC designed for integrated satellite control and data processing applications. It combines a Cortex-A9 processor core with a DSP digital signal processor, floating-point processor, and multiple communication interfaces including 1553B, CAN, and SpaceWire buses, as well as a DMA controller. The chip achieves performance exceeding 1000 MIPS @ 500 MHz, with power consumption below 3 W, reaching advanced international standards.

Key Specifications

ParameterValue
Process Technology0.13 μm
Dimensions (mm)41 × 41 × 10
Weight (g)12
Operating Temperature (°C)−55 to +125
Storage Temperature (°C)−65 to +150
Communication InterfaceSpaceWire / 1553B / CAN / RS-422
Package TypeCCGA1153
Quality GradeCAST C

Key Features

  • High functional integration with Cortex-A9 and DSP cores, floating-point processor, and 1553B, CAN, and SpaceWire interfaces.
  • High computational performance exceeding 1000 MIPS @ 500 MHz.
  • Excellent radiation tolerance with triple modular redundancy and radiation-hardened unit design.
  • Independently developed and fully controllable technology.

Applications

  • Used in satellite control management and image data processing systems, research completed in 2016.

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Frequently Asked Questions

Common questions about SoC2016 32-bit Space Application On-Chip System

What processing architecture does the SoC2016 use?

The SoC2016 is a heterogeneous multi-core SoC combining a Cortex-A9 processor core with a DSP, a floating-point processor, and a DMA controller, achieving over 1000 MIPS at 500 MHz.

Which communication interfaces does the SoC2016 support?

It supports SpaceWire, 1553B, CAN, and RS-422 buses, making it suitable for integrated satellite control and image data processing.

What is the power consumption and package of the SoC2016?

Power consumption is below 3 W. The chip is supplied in a CCGA1153 package at CAST C grade, measuring 41 x 41 x 10 mm and weighing about 12 g.

How is the SoC2016 protected against radiation?

It uses triple modular redundancy and radiation-hardened unit design, and its development was completed in 2016 for satellite control management and image data processing systems.

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