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.
Keep this discovery
Explore connections, maps & timelines
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
Cite the original work for its findings. Save a collection to share your selection of sources.