Visual Overview
Technical Details
Comprehensive specifications and technical information
XY6664RH Radiation-Resistant 8K×8bit PROM
Quick Overview
The XY6664RH is a programmable read-only memory (PROM) chip developed with 0.18 μm CMOS technology. It offers high performance, radiation resistance, and low power consumption. The device is equipped with a dedicated programmer supporting both manual and automatic programming. It is suitable for aerospace electronics and control applications.
Key Specifications
| Parameter | Value |
|---|---|
| Process Technology | 0.18 μm |
| Dimensions (mm) | 35.5 × 15.5 × 3 |
| Weight (g) | 4.7 |
| Operating Temperature (°C) | −55 to +125 |
| Storage Temperature (°C) | −65 to +150 |
| Package Type | CDIP28 |
| Quality Grade | CAST C |
Key Features
- Programmable and read-only operation.
- 8K×8bit storage capacity.
- Strong radiation resistance.
- Fully independent and controllable design.
Applications
- Used in aerospace embedded electronic systems, first flight planned for 2019.
Related Products
- See related products in this series
Documentation & Resources
Frequently Asked Questions
Common questions about XY6664RH Radiation-Resistant 8K×8bit PROM
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.