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Structural considerations for fabrication and mounting of the AXAF HRMA opticsA methodology is described which minimizes optics distortion in the fabrication, metrology, and launch configuration phases. The significance of finite element modeling and breadboard testing is described with respect to performance analyses of support structures and material effects in NASA's AXAF X-ray optics. The paper outlines the requirements for AXAF performance, optical fabrication, metrology, and glass support fixtures, as well as the specifications for mirror sensitivity and the high-resolution mirror assembly. Analytical modeling of the tools is shown to coincide with grinding and polishing experiments, and is useful for designing large-area polishing and grinding tools. Metrological subcomponents that have undergone initial testing show evidence of meeting force requirements.
Document ID
19910052038
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cohen, Lester M.
(Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Cernoch, Larry
(Hughes Danbury Optical Systems, Inc. CT, United States)
Mathews, Gary
(Eastman Kodak Co. Rochester, NY, United States)
Stallcup, Michael
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Advances in Optical Structure Systems
Location: Orlando, FL
Country: United States
Start Date: April 16, 1990
End Date: April 19, 1990
Accession Number
91A36661
Distribution Limits
Public
Copyright
Other

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