InnaLabs® Awarded Space Contracts by Space Primes
InnaLabs® has been awarded the contract for the European Space Agency (ESA) Copernicus LSTM Science...
Additional product specifications, outline drawings and block diagrams, and test data are available on request.
|One-year Composite Repeatability||µg||≤80|
|Scale Factor||mA/g||1.2 to 1.46|
|One-year stability (3-sigma)||ppm||≤70|
|One-year stability (3-sigma)||µrad||
|Vibration Rectification||µg/g2 RMS||
≤15 (DC-500 Hz)
≤40 (500 - 2,000 Hz)
|Intrinsic Noise||µg RMS||≤7 (0-10 Hz)
≤70 (10-500 Hz)
≤1,500 (500-10,000 Hz)
|Operating Temperature||°C||-55 to +95|
|Shock survival (half-sine)||g, ms||500 g @ 0.5ms|
|Vibration Peak Sine||g, Hz||15g @ 20 to 2,000 Hz|
|Quiescent Current per Supply||mA||≤36|
|Quiescent Power @±15VDC||W||≤1.1|
|Input Voltage||VDC||±13 to ±18|
|Diameter||mm||Ø 25.45 Max|
|Case Material||300 Series Stainless Steel|
Its main application is navigation and Fault Detection Isolation and Recovery (FDIR) onboard satellites as well as for land, marine, and aerospace applications.
Browse our library of inertial sensor technical papers for an in-depth view of our Quartz Pendulous Accelerometers.
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 questions? Evaluations and low volume deliveries are available quickly and our sales team are waiting to hear from you.
InnaLabs® offers a range of gyroscopes, accelerometers and systems based on the same design and production processes.