| タイトル | Partial polarizer filter |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790006720 |
| 著者（英） | Title, A. M. |
| 著者所属（英） | NASA Goddard Space Flight Center|Lockheed Missiles and Space Co. |
| 発行日 | 1978-12-12 |
| 言語 | eng |
| 内容記述 | A 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. |
| NASA分類 | OPTICS |
| レポートNO | 79N14891 |
| 権利 | No Copyright |
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