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Compact Inertial Reference Unit for Space (Cirus - A)

The CIRUS-A system features three Fiber-Optic Gyro (FOG) sensors with three accelerometers integrated with industrial-grade electronic components in a durable package. 

 The CIRUS-A can also be configured with radiation-hardened components, if required.


 Applications include:  
  • Platform/gimbal stabilization
  • Pointing applications
  • Missile guidance systems
  • Vehicle/platform navigation
  • Northfinder applications 

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