Compact Inertial Reference Unit for Space

CIRUS

CIRUS-EX

A next-generation strategic-grade Fiber Optic Gyro (FOG) Inertial Reference Unit for spacecraft attitude control — four fully redundant gyros, rad-hard electronics, and dual-redundant interfaces built on more than 60 years of space heritage.

0.0003°/hr bias stability  ·  < 0.000190°/√hr random walk (EOL)  ·  34 lb weight
0.0003°/hr bias stability  ·  < 0.000125°/√hr random walk (EOL)  ·  37 lb weight
0.0003°/hr
Bias Stability
< 0.000190°/√hr
Random Walk (EOL)
> 30°/sec
Angular Rate Range
34 lb
Weight
≤ 40 W
Power
0.0003°/hr
Bias Stability
< 0.000125°/√hr
Random Walk (EOL)
> 22°/sec
Angular Rate Range
37 lb
Weight
≤ 40 W
Power
CIRUS Compact Inertial Reference Unit for Space
The Hardware

Four gyros, one integral chassis

Leveraging over sixty years of experience and proven performance in systems deployed in space, CIRUS is designed and qualified as the next-generation product of our heritage system. CIRUS and CIRUS-EX rate sensors deliver two different strategic grades of performance combined with the benefits of a compact, low-cost system in an integral chassis — four Fiber Optic Gyro (FOG) sensors operating in a fully redundant configuration for spacecraft attitude control, supporting DoD, NASA, and commercial missions.

4× FOG Sensors Rad-Hard Electronics Dual-Redundant Interfaces
Key Performance Features

Built for mission success

Cost-effective, next-generation, strategic-grade Fiber Optic Gyros — engineered for flexibility, reliability, and adaptability across changing mission environments.

Precision & Redundancy

  • Two performance grades with lowest ARW <100 µ°/√hr
  • Four gyros & dual A/B electronics for optimal redundancy
  • High-reliability Class S & Class K rad-hard electronics

Flexible Interfaces

  • Dual-redundant serial interfaces (MIL-STD-1553 & RS-422)
  • Each sensor individually power-selectable
  • Telemetry format customizable for any user interface

Mission Adaptability

  • User-selectable thermal set points
  • User-selectable "on-station" command execution
  • Conductive or radiative vehicle-mount options
Applications

Where CIRUS performs

Where CIRUS-EX performs

Built on more than 60 years of space heritage, the CIRUS family delivers mission-critical precision pointing and navigation for spacecraft attitude control, missile guidance, and platform navigation.

Spacecraft Attitude Control

Spacecraft Attitude Control Platform

  • DoD, NASA & commercial missions
  • Fully redundant FOG configuration
Missile Guidance

Missile Guidance Systems

  • Strategic & tactical guidance
  • Inertial navigation & pointing
Stabilization Pointing Applications Vehicle / Platform Navigation Northfinder Applications
PDF
CIRUS & CIRUS-EX Datasheet
Technical data is available only after review by Aerosphere.
Request Technical Data
Get in touch

Talk to an inertial
sensing engineer

From datasheet questions to evaluation units, our team can help scope CIRUS or CIRUS-EX for your mission.

×
Technical resources

Request a datasheet

Tell us where to send the datasheet. Email and company are required.

We’ll use these details to respond to your datasheet request.

Thank you. Your datasheet request has been received. Our team will follow up by email.
Your request could not be sent. Please check your details and reCAPTCHA, then try again.