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Comprehensive specifications and technical information
Quad-Core SoC2012 32-bit Space Application On-Chip System
Quick Overview
The SoC2012 is the first domestically developed high-performance quad-core SoC designed for satellite onboard computing. It integrates four SPARC V8 cores with a total processing performance exceeding 300 MIPS and 75 FLOPS @ 100 MHz. With a power consumption below 1 W, the SoC2012 outperforms comparable European and American products, achieving world-class performance levels for satellite applications.
Key Specifications
| Parameter | Value |
|---|---|
| Process Technology | 0.13 μm |
| Dimensions (mm) | 37 × 37 × 3 |
| Weight (g) | 12 |
| Operating Temperature (°C) | −55 to +125 |
| Storage Temperature (°C) | −65 to +150 |
| Communication Interface | 1553B / RS-422 |
| Package Type | CQFP256 |
| Quality Grade | CAST C |
Key Features
- High functional integration with four V8 processor cores, floating-point unit, and 1553B bus controller.
- High computational performance exceeding 300 MIPS @ 100 MHz.
- Excellent radiation tolerance with triple modular redundancy and radiation-hardened units.
- Independently developed and fully controllable technology.
Applications
- Microsatellites and embedded electronic systems requiring high-performance onboard computing, first flight in 2015.
Related Products
- See related products in this series
Documentation & Resources
Frequently Asked Questions
Common questions about Quad-Core SoC2012 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.