NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
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
19990093139
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
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)
Escobedo, Javier
(Composite Optics, Inc. San Diego, CA United States)
Kasl, Eldon P.
(Composite Optics, Inc. San Diego, CA United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1999
Subject Category
Structural Mechanics
Report/Patent Number
L-17881
NAS 1.15:209682
NASA/TM-1999-209682
Funding Number(s)
PROJECT: RTOP 632-10-14
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available