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Technical Details
Comprehensive specifications and technical information
SoC2016 32-bit Space Application On-Chip System
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 and 500 FLOPS @ 500 MHz, with power consumption below 3 W, reaching advanced international standards.
Key Specifications
| Parameter | Value |
|---|---|
| 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 |
| Package Type | CCGA1153 |
| Quality Grade | CAST 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 FLOPS @ 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.
Related Products
- See related products in this series
Documentation & Resources
Frequently Asked Questions
Common questions about SoC2016 32-bit Space Application On-Chip System
What spacecraft platforms is this system compatible with?
This system is compatible with microsatellites, nanosatellites, CubeSats, and larger spacecraft platforms. It features modular design with standard interfaces for easy integration into various mission architectures and supports both commercial and scientific applications.
How does this system enhance spacecraft capabilities?
The system provides advanced functionality with reduced size, weight, and power consumption. It offers improved reliability through redundancy, radiation tolerance, and proven space-qualified components with extensive flight heritage.
What are the key performance specifications?
Key specifications include low power consumption, wide operating temperature range, high radiation tolerance (TID >100 krad), compact form factor, and long operational lifetime (>10 years). The system meets all relevant space qualification standards.
How is system integration and testing performed?
We provide comprehensive integration support including detailed interface specifications, test procedures, and simulation tools. All systems undergo thorough environmental testing, functional verification, and compatibility validation before delivery.
What documentation and support is available?
Complete technical documentation includes user manuals, interface control documents, test reports, and application notes. Our engineering team provides integration support, training, and ongoing technical assistance throughout the mission lifecycle.