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Hybrid Electrostatic/Flextensional Mirror for Lightweight, Large-Aperture, and Cryogenic Space TelescopesA lightweight, cryogenically capable, scalable, deformable mirror has been developed for space telescopes. This innovation makes use of polymer-based membrane mirror technology to enable large-aperture mirrors that can be easily launched and deployed. The key component of this innovation is a lightweight, large-stroke, cryogenic actuator array that combines the high degree of mirror figure control needed with a large actuator influence function. The latter aspect of the innovation allows membrane mirror figure correction with a relatively low actuator density, preserving the lightweight attributes of the system. The principal components of this technology are lightweight, low-profile, high-stroke, cryogenic-capable piezoelectric actuators based on PMN-PT (piezoelectric lead magnesium niobate-lead titanate) single-crystal configured in a flextensional actuator format; high-quality, low-thermal-expansion polymer membrane mirror materials developed by NeXolve; and electrostatic coupling between the membrane mirror and the piezoelectric actuator assembly to minimize problems such as actuator print-through.
Document ID
20130009454
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Patrick, Brian
(ManTech NeXolve Corp. United States)
Moore, James
(ManTech NeXolve Corp. United States)
Hackenberger, Wesley
(TRS Technologies, Inc. State College, PA, United States)
Jiang, Xiaoning
(TRS Technologies, Inc. State College, PA, United States)
Date Acquired
August 27, 2013
Publication Date
January 1, 2013
Publication Information
Publication: NASA Tech Briefs, January 2013
Subject Category
Optics
Report/Patent Number
MFS-32878-1
Report Number: MFS-32878-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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