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Partial polarizer filterA birefringent filter module comprises, in seriatum. (1) an entrance polarizer, (2) a first birefringent crystal responsive to optical energy exiting the entrance polarizer, (3) a partial polarizer responsive to optical energy exiting the first polarizer, (4) a second birefringent crystal responsive to optical energy exiting the partial polarizer, and (5) an exit polarizer. The first and second birefringent crystals have fast axes disposed + or -45 deg from the high transmitivity direction of the partial polarizer. Preferably, the second crystal has a length 1/2 that of the first crystal and the high transmitivity direction of the partial polarizer is nine times as great as the low transmitivity direction. To provide tuning, the polarizations of the energy entering the first crystal and leaving the second crystal are varied by either rotating the entrance and exit polarizers, or by sandwiching the entrance and exit polarizers between pairs of half wave plates that are rotated relative to the polarizers. A plurality of the filter modules may be cascaded.
Document ID
19790006720
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Title, A. M.
(Lockheed Missiles and Space Co. Sunnyvale, Calif., United States)
Date Acquired
September 3, 2013
Publication Date
December 12, 1978
Subject Category
Optics
Report/Patent Number
Patent Number: NASA-CASE-GSC-12225-1
Patent Number: US-PATENT-4,129,357
Patent Application Number: US-PATENT-APPL-SN-823566
Accession Number
79N14891
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-GSC-12225-1|US-PATENT-4,129,357
Patent Application
US-PATENT-APPL-SN-823566
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