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Outgassing: Its effects on spacecraft. Vibration damping materialsThe correlation of outgassing to the stability of the damping properties of polymer materials to be used in spacecraft structures is discussed. A test series was devised to obtain basic information from off-the-shelf damping materials. The test results could be considered as a guideline toward the application of these materials. Eight materials were selected to form a representative cross section of those polymers having both ready availability as commercial damping materials and desirable properties. A table indicates the temperatures at which peak damping occurs at 1 Hz and the type of beam specimen used in the vacuum exposure tests. These materials as a group cover the temperature range of -85 C to 38 C.
Document ID
19820017427
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Michael L. Drake
(Dayton Univ. Research Inst. United States)
Matthew F. Kluesener
(Dayton Univ. Research Inst. United States)
William R Goddard
(Dayton Univ. Research Inst. United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Publication Information
Publication: NASA. Goddard Space Flight Center 12th Space Simulation Conf.
Publisher: National Aeronautics and Space Administration
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Twelfth Space Simulation Conference
Location: Pasadena, CA
Country: US
Start Date: May 16, 1982
End Date: May 18, 1982
Sponsors: American Institute for Aeronautics & Astronautics
Accession Number
82N25303
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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