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Scanning mirror for infrared sensorsA high resolution, long life angle-encoded scanning mirror, built for application in an infrared attitude sensor, is described. The mirror uses a Moire' fringe type optical encoder and unique torsion bar suspension together with a magnetic drive to meet stringent operational and environmental requirements at a minimum weight and with minimum power consumption. Details of the specifications, design, and construction are presented with an analysis of the mirror suspension that allows accurate prediction of performance. The emphasis is on mechanical design considerations, and brief discussions are included on the encoder and magnetic drive to provide a complete view of the mirror system and its capabilities.
Document ID
19730010161
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, R. H.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Bernstein, S. B.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 7, 2013
Publication Date
November 1, 1972
Publication Information
Publication: NASA. Lyndon B. Johnson Space Center The 7th Aerospace Mech. Symp.
Subject Category
Instrumentation And Photography
Accession Number
73N18888
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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