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A Deployable Primary Mirror for Space TelescopesNASA Langley Research Center, Composite Optics, Inc., and Nyma/ADF have developed jointly a deployable primary mirror for space telescopes that combines over five years of research on deployment of optical-precision structures and over ten years of development of fabrication techniques for optical-precision composite mirror panels and structures. The deployable mirror is directly applicable to a broad class of non-imaging "lidar" (Light direction and ranging) telescopes whose figure-error requirements are in the range of one to ten microns RMS. Furthermore, the mirror design can be readily modified to accommodate imaging-quality reflector panels and active panel-alignment control mechanisms for application to imaging telescopes. The present paper: 1) describes the deployable mirror concept; 2) explains the status of the mirror development; and 3) provides some technical specifications for a 2.55- m-diameter, proof-of-concept mirror.
Document ID
19990064014
Acquisition Source
Langley Research Center
Document Type
Reprint (Version printed in journal)
Authors
Lake, Mark S.
(NASA Langley Research Center Hampton, VA United States)
Phelps, James E.
(NYMA, Inc. Hampton, VA United States)
Dyer, Jack E.
(Composite Optics, Inc. San Diego, CA United States)
Caudle, David A.
(Composite Optics, Inc. San Diego, CA United States)
Tam, Anthony
(Composite Optics, Inc. San Diego, CA United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1999
Subject Category
Optics
Report/Patent Number
Paper-3785
Meeting Information
Meeting: Optical Science, Engineering and Instrumentation
Location: Denver, CO
Country: United States
Start Date: July 18, 1999
End Date: July 23, 1999
Sponsors: International Society for Optical Engineering
Distribution Limits
Public
Copyright
Other

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