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.
Keep this discovery
Explore connections, maps & timelines
Lange, William G., Dietrich, Robert W.. 1990-08-01. The MESA accelerometer for space application. https://ntrs.nasa.gov/citations/19910003100
Cite the original work for its findings. Save a collection to share your selection of sources.