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Characterization of Adhesives for Attaching Reusable Surface Insulation on Space Shuttle VehiclesAn extensive development and testing program on adhesive systems shows that: (1) A closed cell silicone rubber sponge bonded to substrates with thin bond lines of glass filled adhesive exhibits density and modulus values approximately one third that of solid silicone adhesives; (2) utilization of glass or phenolic microballoons as fillers in silicone adhesives reduces density but increases moduli of the vulcanized materials; (3) the silicone elastomer based adhesives appear to be complex systems rather than homogeneous, isotropic materials. Tensile, shear, and compression properties plotted versus temperature verify this conjecture; and (4) constant strain-stress relaxation tests on glass-filled adhesive show that stress relaxation is most pronounced near the glass transition temperature.
Document ID
19730024758
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Owen, H. P.
(General Dynamics/Fort Worth TX, United States)
Carroll, M. T.
(General Dynamics/Fort Worth TX, United States)
Date Acquired
August 7, 2013
Publication Date
September 1, 1973
Publication Information
Publication: NASA. Ames Res. Center Symp. on Reusable Surface Insulation for Space Shuttle, Vol. 3
Subject Category
Materials, Nonmetallic
Accession Number
73N33491
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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