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Scanning mirror design considerations for a geostationary spaceborne radiometerThis paper will address the design considerations and challenges for a radiometer scanning mirror in a Geostationary (GEO) orbit. With increasingly demanding imaging requirements, mirror designs that are insensitive to the harsh thermal environment will be required. The compatibility of various mirror designs for a precision radiometer will be examined and discussed. The design solutions considered will include material, geometry and thermal design tradeoffs.
Document ID
19930045997
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hookman, R. A.
(NASA Headquarters Washington, DC United States)
Zurmehly, G. E.
(NASA Headquarters Washington, DC United States)
Hodgman, N. S.
(ITT Aerospace Communications Div. Fort Wayne, IN, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: Surveillance technologies II; Proceedings of the Meeting, Orlando, FL, Apr. 21-23, 1992 (A93-29980 11-19)
Publisher: Society of Photo-Optical Instrumentation Engineers
Subject Category
Spacecraft Instrumentation
Accession Number
93A29994
Distribution Limits
Public
Copyright
Other

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