Introducing CVG New Space
With the growing demand for launching new satellite constellations and the expansion of New Space...
POLARIS is an ITAR-free, Single Event Latch-up tolerant and high-performance Inertial Measurement Unit (IMU). It provides to user equipment on a digital RS422 interface, velocity increments and angle increments about three orthogonal measurement axes. Developed with the support of the European Space Agency (ESA), POLARIS is designed for short to medium-term space missions, including launchers, micro-launchers, landers and re-entry vehicles for which the driving issue is robustness to SEE, reliability and meeting performance at a reduced cost and size.
Additional product specifications, outline drawings and block diagrams, and test data are available on request.
The core Gyro technology used in POLARIS is InnaLabs® patented and proven solid-state CVG technology (Coriolis Vibratory Gyroscope). InnaLabs® CVGs are inherently stable, impervious to aging effects in space missions, low mass, low power consumption and achieve outstanding Angular Random Walk.
The CVG perfectly balances with InnaLabs® miniature fused Quartz pendulous accelerometers. These accelerometers are derived from InnaLabs® AI-Q-550, which is an aerospace-grade design delivering dub-milli-g long term stability in high-dynamic environments.
POLARIS will be released to market by Q4 2024.
|Measurement Range||±400°/s, ±40g|
|Bandwidth||≥ 100 Hz|
|Data Interface||RS422 Data Interface, Asynchronous|
|Settable output data rate||200 Hz nominal|
|Supply voltages||15 VDC|
|Power Consumption||10 W|
|Diameter||112 mm x 132 mm x 145 mm (Height)|
|Mass||≤ 2 kg|
|Temperature||-45°C (-49°F) to +85°C (+45°F)|
|Shocks, SRS||10,000 g - 2kHz, Q=10|
|Random Vibrations||≥ 14.5 g rms|
|Angular Random Walk||≤ 0.01°/√hr|
|In-run bias||≤ 0.3 °/hr (1σ)|
|Bias erros (temp.)||≤1 °/hr (1σ) (BOL)|
|Scale Factor errors (all effects)||≤ 500 ppm (BOL)|
|MTBF||≥30,000 hr (GM), ≥5,000 (RL)|
≤ 100 µ.s/√hr (i.e. 0.001 (m/s)/√hr)
|In-run bias||≤ 10 µg (1σ)|
|Bias erros (temp.)||≤ 300 µg (1σ) (BOL)|
|Scale Factor errors (all effects)||≤ 500 ppm (1σ)|
POLARIS can be used in many space applications.
Browse our library of inertial sensor technical papers for an in-depth view of our technology.
InnaLabs® have the technology and 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 questions? Evaluations and low volume deliveries are available quickly and our sales team are waiting to hear from you.
InnaLabs® Inertial Sensors are available in a number of form factors.