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NASA NTRS · 19720023230

Status of reusable surface insulation thermal protection system technology programs

Abstract

The development of three low-density rigidized insulation materials for the shuttle TPS application is reported. These materials consist of one high purity silica system and two systems based on mullite, an aluminum silicate. Both systems consist of fibers joined together with appropriate binders to obtain a rigidized insulation composite. Both material systems require the application of a glassy coating to provide a wear resistant, high emittance surface and to prevent the absorption of water by the fiber matrix. The technology program has addressed the development of water impervious coatings, methods of assembling the materials in design concepts while minimizing the thermal stress in the insulation, achieving compatibility between the RSI material and the structural system, and test evaluations to demonstrate the feasibility of the surface insulation concept.

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Greenshields, D. H., Meyer, A. J., Tillian, D. J.. 1972-07-01. Status of reusable surface insulation thermal protection system technology programs. https://ntrs.nasa.gov/citations/19720023230

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