ATA Sensors ARS-12A angular rate sensor

Product Description

ATA Sensors ARS-12A MHD Angular Rate Sensor – Precision Inertial Sensor for Stabilization and Pointing Applications

This used ATA Sensors ARS-12A is a high-performance inertial angular rate sensor based on Magnetohydrodynamic (MHD) technology. ATA Sensors, formerly the commercial division of Applied Technology Associates, developed this sensor to provide exceptional wideband angular motion measurement capabilities.

According to SBIR documentation from the Environmental Protection Agency, the Model ARS-12 was recognized as an innovative product possessing the appropriate size, bandwidth, measurement noise, dynamic range, ruggedness, and cost characteristics desired for aircraft optical reference applications . The ARS-12 series was developed in support of U.S. Air Force requirements for a small, inexpensive inertial attitude reference system that functions as a two-axis optical reference in high-performance aircraft .

⚠ IMPORTANT EXPORT CONTROL NOTICE:
This item is subject to International Traffic in Arms Regulations (ITAR) or Export Administration Regulations (EAR). It may not be sold or transferred to foreign persons or entities without proper U.S. Government export authorization. This item is available for domestic sale within the United States ONLY. Prior to purchase, BMI Surplus may require verification of end-user eligibility. All applicable export control laws and regulations apply.

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Key Specifications

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About MHD Sensor Technology

MHD angular rate sensors offer distinct advantages over traditional rate gyroscopes :

• Wide Bandwidth: Capable of measuring high-frequency angular motion from 1Hz to 1,000Hz

• Low Noise: Exceptional sensitivity (<25 nanoradians) for precision stabilization

• No Moving Parts: Solid-state design for high reliability

• Rugged Construction: Withstands 1,000g shock, -60°C to +85°C temperature range

• Space Qualified: Proven performance in aerospace environments

The ARS-12 was specifically identified for use in isolating a telescope’s optical line-of-sight (LOS) from aircraft base motion, achieving LOS jitter of 3 microradians or less . The sensor was developed with support from the U.S. Air Force High Altitude Balloon Experiment (HABE) program .

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Applications

• Aircraft Optical Reference: Line-of-sight stabilization for airborne telescopes and sensors

• Space Qualified Systems: Satellite and spacecraft pointing applications

• Jitter Elimination: Designed to eliminate jitter from airborne mirrors, optics, and lasers

• Precision Pointing Systems: Jitter measurement and active vibration cancellation

• Inertial Navigation: Augmentation of conventional gyro systems

• Legacy System Support: Replacement or spare for existing ATA sensor installations

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Condition

SOLD AS IS
USED – SHOWS NORMAL HANDLING
FUNCTIONALITY NOT TESTED
NO CABLE, CONTROLLER, OR DOCUMENTATION INCLUDED
PICTURE MAY NOT MATCH PRODUCT

⚠ SENSITIVE ELECTRONICS NOTE: This sensor contains precision electronic components. Handle with care to avoid damage from electrostatic discharge (ESD) or mechanical shock.