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Mechanical component screening for scannerThe critical mechanical components of the scan mirror mechanism are described and their evaluation and screening procedures are discussed. A bumper/damper unit is used in the design to reverse motion of the mirror and effect scan and retrace cycles. A wear evaluation was conducted on the bumper impact surfaces that established nylon 6-10 as an acceptable material. The elastomeric dampers were subjected to thermal vacuum tests for condensables and outgassing as well as parametric life tests. The flexure pivots that support the mirror were tested to establish a curve of stress plotted as a function of cycles to failure for rotational operation. The pivots met the life requirement of 150,000,000 cycles at a + or - 2.9 deg amplitude during fatigue testing. Screening procedures were established for dampers and flexure pivots to obtain flight quality components.
Document ID
19730010145
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Olson, J. L.
(Hughes Aircraft Co. Culver City, CA, United States)
Quinn, W. J.
(Hughes Aircraft Co. Culver City, 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
73N18872
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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