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Planetary-Whigs: Optical MEMS-Based Seismometer

Completed TRL 4 (started at 3, targeting 4)

Description

During this Phase I, Michigan Aerospace Corporation will adapt the design of an optical MEMS seismometer for lunar and other planetary science instrumentation. The optical MEMS based seismometer takes advantage of the high Q of morphological dependent resonances and can be sensitive to a few nano-g with a proof mass under 80 grams. The three-axis seismometer, originally designed for field applications, will be rugged, compact and low power (<160 mW per channel). During the Phase I effort, MAC will develop the design for the instrumentation, with specific attention to the environmental conditions encountered on the lunar surface, in particular the large temperature excursions and galactic cosmic radiation. During Phase II, an engineering model will be fabricated, tested and demonstrated.

Benefits

This effort will produce a design for a compact, low-power optical MEMS-based seismometer that will be rugged enough for use on the Moon; such a device will find use for seismic sensing on other solar system bodies as NASA missions explore asteroids, Mars and elsewhere. The sensitivity of the device is such that it can be used for sensitive studies of acceleration in spacecraft, for example to study atmospheric drag on satellites. Extremely rugged sensors normally used for space applications will also find terrestrial work in seismic studies near active volcanoes and other extreme Earth-bound environments.

The base technology will result in low-cost accelerometers, no matter the application. The components are inexpensive, and the fabrication and packaging do not require highly-specialized environments, unlike micro-fabricated devices. We anticipate such instrument to penetrate the market because its reliability and affordability. Applications for such an accelerometer encompass a broad range of activities. They include: --Geological research: mining and oil prospecting --Earth sciences --Space exploration: satellite drag measurements, docking, navigation --Homeland security: footstep detection, tampering, entry and illicit activities --Building safety --Academic research --Vehicle safety research

Details

Technology areaCommunications, Navigation, and Orbital Debris Tracking and Characterization Systems > Optical Communications > Optimetrics
ProgramSmall Business Innovation Research/Small Business Tech Transfer (SBIR/STTR)
Lead organizationMichigan Aerospace Corporation, Ann Arbor, MI
Start date2012-02-23
End date2012-08-23

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This is early/mid-stage (TRL 4) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.

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