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NASA Scientific and Technical Aerospace Reports

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20040120996 <strong>NASA</strong> Marshall Space Flight Center, Huntsville, AL, USA<br />

Magnetic Symbology Reader<br />

Schramm, Harry F., Inventor; Shih, William C. L., Inventor; Fitzpatrick, Gerald L., Inventor; Knisely, Craig, Inventor; June<br />

08, 2004; 5 pp.; In English; Original contains black <strong>and</strong> white illustrations<br />

Patent Info.: Filed 5 Aug. 2002; US-Patent-6,745,942; US-Patent-Appl-SN-214482; <strong>NASA</strong>-Case-MFS-31768-1; No<br />

Copyright; Avail: CASI; A01, Hardcopy<br />

A magnetic symbology reader has a housing containing a polarized light source which directs light though a<br />

magneto-optic sensor onto a reflector which reflects light least one analyzer <strong>and</strong> into at least one camera. A view finder allows<br />

the user to monitor the image on the sensor as seen by a viewfinder camera while a processor is coupled to possibly a second<br />

camera so that when an image is detected, the image from the camera may be processed by the processor to output information<br />

associated with the symbol to an external source. The analyzer <strong>and</strong> polarized light source provide contrast in the images<br />

detected by the sensor. A bias/erase coil located about the magneto-optic sensor can enhance or erase images on the sensor.<br />

Official Gazette of the U.S. Patent <strong>and</strong> Trademark Office<br />

Magneto-Optics; Readers; Symbols; Sensors<br />

20040121090 <strong>NASA</strong> Marshall Space Flight Center, Huntsville, AL, USA<br />

A Novel <strong>and</strong> New Ultra-Lightweight Reinforcement for Producing Low Mass Optical Systems<br />

Kobell, W.; [2004]; 1 pp.; In English; Mirror Technology Days (SD70 Website), 17-19 Aug. 2004, Huntsville, AL, USA<br />

Contract(s)/Grant(s): NAS8-00199; No Copyright; Avail: CASI; A01, Hardcopy<br />

This Phase II SBIR project deals with the manufacturing of isotropic, hollow carbon fibers for optical applications. The<br />

intrinsic CTE anisotropy of carbon fibers makes them virtually impractical for optical applications. A novel approach to this<br />

problem was implementation of carbon fibers that are isotropic <strong>and</strong> have good mechanical properties. A 4’ deliverable mirror<br />

was fabricated with this fiber <strong>and</strong> delivered to <strong>NASA</strong> MSFC. Optical quality Silicon was applied to the surface. Subsequently,<br />

1/5 wave P/V was achieved. Currently a 18’ optic is being fabricated with this fiber.<br />

Author<br />

Carbon Fibers; Isotropy; Mass; Optical Equipment<br />

20040121119 Bennett Optical Research, Inc., Ridgecrest, CA, USA<br />

Fabrication <strong>and</strong> Testing of Active <strong>and</strong> Adaptive Cyanate Ester Composite Mirrors<br />

Bennett, H. E.; [2004]; 1 pp.; In English; Miror Technology Days (SD70 Website), 17-19 Aug. 2004, Huntsville, AL, USA<br />

Contract(s)/Grant(s): NAS8-02008; No Copyright; Avail: Other Sources; Abstract Only<br />

The objective of the <strong>NASA</strong>/Bennett Optical Research Inc. (BOR) NAS8-02008 Phase II Program, which also<br />

incorporated ideas developed under the earlier <strong>NASA</strong> NAS8-01035 Phase 1 Program, was to develop a large mirror fabrication<br />

<strong>and</strong> test facility with emphasis on producing large, light weight active <strong>and</strong> adaptive optics. A principle objective was to develop<br />

m<strong>and</strong>rels on which to make large composite graphite-filled cyanate ester mirrors, Deliverables were two of these superpolished<br />

lightweight active/adaptive optic composite mirrors, one 12’ (approx.1/3 meter) in diameter <strong>and</strong> one 22’ (approx.1/2 meter)<br />

in diameter. In addition optical superpolishers for m<strong>and</strong>rels up to 1.2 meters in diameter, test instruments for determining<br />

optical figure <strong>and</strong> scattered light, novel design actuators for making the composite mirrors both active <strong>and</strong> adaptive, <strong>and</strong><br />

passive <strong>and</strong> active means for measuring actuator performance were developed at BOR. We are now installing a superpolisher<br />

capable of producing 3 meter diameter mirror/m<strong>and</strong>rels. All polishers utilize the principle of centrifugal elutriation <strong>and</strong><br />

produce superpolished m<strong>and</strong>rels with surface microroughnesses under 1 nm rms.<br />

Author<br />

Adaptive Optics; Fabrication; Mirrors; Test Facilities<br />

75<br />

PLASMA PHYSICS<br />

Includes magnetohydrodynamics <strong>and</strong> plasma fusion. For ionospheric plasmas see 46 Geophysics. For space plasmas see 90<br />

Astrophysics.<br />

20040111048 <strong>NASA</strong> Johnson Space Center, Houston, TX, USA<br />

ISS Plasma Interaction: Measurements <strong>and</strong> Modeling<br />

Barsamian, H.; Mikatarian, R.; Alred, J.; Minow, J.; Koontz, S.; 8th Spacecraft Charging Technology Conference; March<br />

2004; 9 pp.; In English; See also 20040111031; No Copyright; Avail: CASI; A02, Hardcopy<br />

294

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