A monolithic high-g SOI-MEMS accelerometer for measuring projectile launch and flight accelerations

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Abstract

Analog Devices (ADI) has designed and fabricated a monolithic high-g acceleration sensor (ADXSTC3-HG) fabricated with the ADI silicon-on-insulator micro-electro-mechanical system (SOI-MEMS) process. The SOI-MEMS sensor structure has a thickness of 10 um, allowing for the design of inertial sensors with excellent cross-axis rejection. The high-g accelerometer discussed in this paper was designed to measure in-plane acceleration to 10,000 g while subjected to 100,000 g in the orthogonal axes. These requirements were intended to meet Army munition applications. The monolithic sensor was packaged in an 8-pin leadless chip carrier (LCC-8) and was successfully demonstrated by the US Army Research Laboratory (ARL) as part of an inertial measurement unit during an instrumented flight experiment of artillery projectiles launched at 15,000 g. © 2006 - IOS Press and the authors. All rights reserved.

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Davis, B. S., Denison, T., & Kuang, J. (2006). A monolithic high-g SOI-MEMS accelerometer for measuring projectile launch and flight accelerations. Shock and Vibration, 13(2), 127–135. https://doi.org/10.1155/2006/793564

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