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NASA NTRS · 19730024736

Optimization of Rei-mullite Physical Properties

Abstract

Micromechanical and thermal modeling studies prove that ceramic fiber mullite materials is the only system capable of shuttle thermal protection to 1644 K. Hafnia pigmentated mullite surface coatings meet both orbital and reentry thermal radiative requirements for reuse without refurbishment. Thermal and mechanical models show growths potentials associated with the mullite system for a factor of 2 improvement in mechanical properties, and a factor of 2 to 3 reduction in thermal conductivity.

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Tanzilli, R. A., Musikant, S., Bolinger, P. N., Brazel, J. P.. 1973-09-01. Optimization of Rei-mullite Physical Properties. https://ntrs.nasa.gov/citations/19730024736

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