Visual Overview
Technical Details
Comprehensive specifications and technical information
Metal Coriolis Vibratory Gyroscope (CVG)
Quick Overview
The Metal Coriolis Vibratory Gyroscope (CVG) is widely used in weapon-mounted systems, attitude stabilization platforms, and space applications (e.g., Google, ESA, OneWeb).
Key Specifications
| Parameter | Value |
|---|---|
| Dimensions (mm) | B110 × L110 × H90 |
| Weight (g) | 1000 |
| Power Consumption | ≤ 6 W |
| Communication Interface | RS-422 |
| Design Life | 8 years |
| Bandwidth | ≥ 20 Hz |
| Bias | ≤ 5 °/h |
| Bias Stability (1σ, full temperature) | ≤ 10 °/h |
| Bias Repeatability (1σ) | ≤ 1 °/h |
| Bias Instability (1σ) | ≤ 0.1 °/h |
| Angle Random Walk | ≤ 0.007 °/√h |
| Measurement Range | −20°/s to +20°/s |
| Scale Factor | 10,000 LSB/°/s |
Key Features
- High reliability
- Space-qualified
Applications
- Used for attitude sensing, stabilization, and control in satellite constellations, aerospace systems, and space-grade inertial navigation platforms.
Related Products
- See related products in this series
Documentation & Resources
Frequently Asked Questions
Common questions about Metal Coriolis Vibratory Gyroscope (CVG)
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.