Payload characterization for CubeSat demonstration of MEMS deformable mirrors

Payload characterization for CubeSat demonstration of MEMS deformable mirrors

Coronagraphic space telescopes require wavefront control systems for high-contrast imaging applications such as exoplanet direct imaging. High-actuator-count MEMS deformable mirrors (DM) are a key element of these wavefront control systems yet have not been flown in space long enough to characterize...

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Bibliographic Details
Main Authors: Cahoy, Kerri (Contributor), Belikov, Ruslan (Author), Bendek, Eduardo (Author), Marinan, Anne D. (Contributor), Webber, Matthew William (Contributor)
Other Authors: Massachusetts Institute of Technology. Department of Aeronautics and Astronautics (Contributor), Massachusetts Institute of Technology. Department of Earth, Atmospheric, and Planetary Sciences (Contributor)
Format: Article
Language:English
Published: SPIE, 2015-05-05T18:00:55Z.
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