THERMAL PROPERTIES OF ABLATIVE CHARS
Abstract
The objective of this program was to determine thermal conductivity, specific heat, thermal expansion and density to 4500F on well-defined samples of charred phenolic-carbon and phenolic-graphite ablators. Methods were to be established for characterizing chars of three phenolic carbon or phenolic graphite ablators from tested full scale hardware. Then methods for producing stable duplicates of three zones between 1200 and 4500F in each char were to be developed. Samples of each of these zones and the virgin ablator were to be produced for measurement of thermal conductivity, specific heat and thermal expansion by Battelle Memorial Institute. Properties parallel to and perpendicular to the laminate were to be determined from room temperature to 700F on virgin material and between 1200 and 4500F on chars. Properties for the unstable pyrolysis zone were to be derived by extrapolation guided by characterization and heat transport theory.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1968
- Accession Number
- AD0675179
Entities
People
- J. E. Cotton
- Paul B. Kennedy
- Robert J. Evans
- T. J. Fabish
- Wilson A. Clayton
Organizations
- Boeing