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SBIR/STTR

Miniaurizable, High Performance, Fiber-Optic Gyroscopes for Small Satellites, Phase I

Completed Technology Project

Project Introduction

Miniaurizable, High Performance, Fiber-Optic Gyroscopes for Small Satellites, Phase I
Small satellites require much lighter weight, smaller, and long life Attitude control components that can withstand stressing launch conditions and space vibration environments without compromising their performance. In particular, rate sensors that can provide high-resolution Line of Sight (LOS) stabilization, accurate inertial pointing and higher bandwidths are needed to support attitude and position determination from highly compact and very lightweight packages. More »

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A final report document may be available for this project. If you would like to request it, please contact us.

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