IMPROVED GRAPHITE MATERIALS FOR HIGH-TEMPERATURE AEROSPACE USE. VOLUME 2. DEVELOPMENT OF GRAPHITE-REFRACTORY COMPOSITES

Abstract

New graphite-base refractory composites were developed through the selective substitution of the components in grade JTA. Studies were conducted on the following composite changes: zirconium, silicon and niobium replacement of boron; and niobium, cerium and lanthanum replacement of silicon. Studies of graphite-oxide reactions have provided information concerning the stability of oxide coatings in contact with carbon bodies. The most oxidation-resistant composite was JT-0981 in which the boron was completely replaced with silicon. This material exhibited excellent performance at 1700, 1800, 1900, and 2000C; however, at lower temperatures, no protective coating was formed and the performance was poor. Plasma tests conducted at 1900C on the front face of JTA samples shows its excellent oxidation resistance. Similar tests on JT-0981 were stopped when the low temperature areas on the samples were losing material faster than the hot face.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1964
Accession Number
AD0609247

Tags

Communities of Interest

  • Advanced Electronics
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Air Force
  • Body Weight
  • Ceramic Materials
  • Chemical Synthesis
  • Chemistry
  • High Temperature
  • Isotherms
  • Low Temperature
  • Materials
  • Materials Laboratories
  • Materials Processing
  • Materials Science
  • Materials Testing
  • Oxidation
  • Oxidation Resistance
  • Oxides
  • Physical Properties

Fields of Study

  • Materials science

Readers

  • Surface Engineering/Surface Coating Technology.

Technology Areas

  • Space