NASA NTRS · 19740022819
Introduction to the adhesive bonding session
Abstract
Space shuttle unique requirements call for the development of a specific adhesive system to reliable attach reusable surface insulation. A low density foam system has been developed that provides strain isolation from the support structure and remains structurally stable in space shuttle thermal environment. Surface preparation and its stabilization by an adhesive primer system are the most important factors in preventing corrosion from reducing the reliability and durability of the adhesive bonding component.
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Mccarty, J. E.. 1972-12-01. Introduction to the adhesive bonding session. https://ntrs.nasa.gov/citations/19740022819
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