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Materials and design for ablative heat shieldsThe goal of the ablation technology program is to bring ablation research and development to a high state of readiness for application to space shuttle vehicles. Some recent results and current work in the areas of materials, designs, and refurbishment for ablative TPS are reported. Future research and development needs are also presented.
Document ID
19720023232
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dow, M. B. (NASA Langley Research Center Hampton, VA, United States)
Tompkins, S. S. (NASA Langley Research Center Hampton, VA, United States)
Coe, F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 6, 2013
Publication Date
July 1, 1972
Publication Information
Publication: NASA Space Shuttle Technol. Conf.
Subject Category
Thermodynamics And Combustion
Accession Number
72N30882
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19720023215Collected WorksNASA Space Shuttle Technology Conference: Dynamics and Aeroelasticity; Structures and MaterialsN72-30865 21-31Collected Works
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