SBIR/STTR Research Award

Enhanced Reliability MEMS Deformable Mirrors for Space Imaging Applications

Award identifier 6dd5e612a7d7aaf2b592df4b5f84a4c0afffc5f1d75807d5000ce734be6f28fdAwarding agency National Aeronautics and Space Administration

Award amount

$99,967

Program and phase

SBIR · Phase I

Award year

2011

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Boston Micromachines Corporation
Proposal award date
2011-02-18
Contract end date
2011-09-29
UEI
SM8TM1GMFMY9
Solicitation number
Not reported
Topic code
S2.02

Research abstract

The goal of this project is to develop and demonstrate a reliable, fault-tolerant wavefront control system that will fill a critical technology gap in NASA's vision for future coronagraphic observatories. The project outcomes include innovative advances in component design and fabrication and substantial progress in development of high-resolution deformable mirrors (DM) suitable for space-based operation.Space-based telescopes have become indispensible in advancing the frontiers of astrophysics. Over the past decade NASA has pioneered coronagraphic instrument concepts and test beds to provide a foundation for exploring feasibility of new approaches to high-contrast imaging and spectroscopy. From this work, NASA has identified a current technology need for compact, ultra-precise, multi-thousand actuator DM devices. Boston Micromachines Corporation has developed microelectromechanical systems (MEMS) DMs that represent the state-of-the-art for scalable, small-stroke high-precision wavefront control. The emerging class of high-resolution DMs pioneered by the project team has already been shown to be compact, low-power, precise, and repeatable. This project will develop a system that eliminates the leading cause of single actuator failures in electrostatically-actuated wavefront correctors Â? snap-through instability and subsequent electrode shorting and/or adhesion. To achieve this we will implement two innovative, complementary modifications to the manufacturing process. We will develop a drive electronics approach that inherently limits actuator electrical current density generated when actuator snap-down occurs, and we will modify the actuator design to mitigate adhesion between contacting surfaces of the actuator flexure and fixed base electrode in the event of snap-down. Phase II research will combine the actuator design and fabrication processes, and current-limiting drive electronics to produce a MEMS DM with 3072 actuators with enhanced reliability.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

38 SBIR/STTR records share this UEI (1999–2024). Reported award amounts total $15,546,351. Reported amounts are not federal obligations.

Phases: Phase II, Phase I

Agencies: National Aeronautics and Space Administration, Department of Defense, Department of Health and Human Services, National Science Foundation

Agency intelligence

National Aeronautics and Space Administration

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