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Spacecraft Systems In Production

Metal Coriolis Vibratory Gyroscope (CVG)

The Metal Coriolis Vibratory Gyroscope (CVG) is used in weapon-mounted systems, attitude stabilization platforms, and space applications.

Metal Coriolis Vibratory Gyroscope (CVG)

Key Specifications

Dimensions (mm)
B110 × L110 × H90
Weight (g)
1000
Power Consumption
≤ 6 W
Communication Interface
RS-422
Design Life
8 years
Bandwidth
≥ 20 Hz
Published: October 16, 2025 Last updated: October 18, 2025
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Comprehensive specifications and technical information

Quick Overview

The Metal Coriolis Vibratory Gyroscope (CVG) is used in weapon-mounted systems, attitude stabilization platforms, and space applications.

Key Specifications

ParameterValue
Dimensions (mm)B110 × L110 × H90
Weight (g)1000
Power Consumption≤ 6 W
Communication InterfaceRS-422
Design Life8 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 Factor10,000 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.

Documentation & Resources

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Frequently Asked Questions

Common questions about Metal Coriolis Vibratory Gyroscope (CVG)

What bias performance does the Metal CVG provide?

The gyroscope offers a bias of no more than 5°/h, bias instability of 0.1°/h, and an angle random walk of 0.007°/√h.

What measurement range and scale factor does it offer?

It measures angular rate from −20 to +20°/s with a scale factor of 10,000 LSB per °/s.

What are the design life and power consumption?

The gyroscope has an 8-year design life and consumes no more than 6 W.

What bandwidth and interface does it use?

It provides a bandwidth of at least 20 Hz and communicates over RS-422, weighing about 1000 g.

What applications is the Metal CVG suited to?

It supports attitude sensing, stabilization, and control in satellite constellations and space-grade inertial navigation platforms.

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