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NASA NTRS · 19910003100

The MESA accelerometer for space application

Abstract

An electrostatically suspended proof mass in the Miniature Electrostatic Accelerometer (MESA) is used to measure acceleration in the submicro-g range. Since no fixed mechanical suspension (such as springs or strings) is used, the constrainment scaling can be changed electrically after being placed in orbit. A single proof mass can sense accelerations in three axes simultaneously. It can survive high-g pyrotechnic-generated shocks and launch environments while unpowered.

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BibTeXRIS

Lange, William G., Dietrich, Robert W.. 1990-08-01. The MESA accelerometer for space application. https://ntrs.nasa.gov/citations/19910003100

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