Introducing CVG New Space
With the growing demand for launching new satellite constellations and the expansion of New Space...
InnaLabs® gyroscopes accumulated over 2.5M hours in space with no failure or degradation of performance.
InnaLabs® Gyroscopes Hours in Space
InnaLabs® Gyroscopes on 19 Satellites
Additional product specifications, outline drawings and block diagrams, and test data are available on request.
|Number of Axes||1 or 2 Axis|
|In-run Bias Stability (room temperature, 1σ), deg/hr||<0.22|
|Bias Stability (full temperature range, 1σ), deg/hr||< 10|
|Scale factor error, full temperature range, 1σ (ppm)||< 3,500|
|Scale factor linearity (ppm)||≤ 1500|
|Angular Random Walk, deg/√hr||0.01 typical|
|Bandwidth (-3dB)||≥ 300|
|Interface||Analogue or Digital RS-422|
|Start-up Time||1 sec typical|
|Weight (each sensitive element)||71 g|
|Weight (each damper)||26 g|
|Weight (each electronics with connectors)||
105 g (One-Axis)
H25 x D29.4
|Built-in Self Test
Explore the whole range of InnaLabs® Space Sensors delivering outstanding performance, no matter the environment.
Browse our library of inertial sensor technical papers for an in-depth view of our Coriolis Vibratory Gyroscopes.
InnaLabs® have the Engineering resources to provide custom solutions to meet your project needs,
with excellent pre and post-sale customer support.
InnaLabs® dedicated and experienced engineers are committed to customer satisfaction by providing innovative technology, quality products, and custom solutions to meet your project needs. More question? Our product team is available to discuss your requirements.