Transverse Expansion of Individual Carbon and Graphite Filaments,

Abstract

The laser diffraction technique for measuring the diameter of fine filaments has been adapted for measuring the transverse coefficient of thermal expansion (CTE) of individual carbon and graphite filaments. CTE was measured on three types of polyacrylonitrile (PAN)-derived filaments and one type of pitch-derived filament that had already been heat-treated to 2600 C. The measurements are unique because the filaments were in a surface-traction-free environment; the data are therefore inherently more accurate than those obtained by conventional methods. Significant variations in the transverse CTE of pitch-based filaments were observed; they have been attributed to local differences in the (transverse) preferred orientation of the graphite layer planes in those filaments. Individual pitch-based filaments were found to twist about their axis when constrained at both ends and heated; the center of the filament presumably undergoes maximum deflection. Keywords: Thermal expansion, Thermal strain, Carbon filaments, Carbon fibers, Composites, Graphite Fibers.

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Document Details

Document Type
Technical Report
Publication Date
Apr 22, 1988
Accession Number
ADA195073

Entities

People

  • Patrick M. Sheaffer

Organizations

  • The Aerospace Corporation

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Carbon Carbon Composites
  • Classification
  • Coefficients
  • Composite Materials
  • Diameters
  • Diffraction
  • Environment
  • Graphitic Materials
  • Heat Treatment
  • High Temperature
  • Materials
  • Materials Science
  • Measurement
  • Orientation (Direction)
  • Security
  • Thermal Expansion
  • Transverse

Fields of Study

  • Physics

Readers

  • Reinforced Composite Materials

Technology Areas

  • Directed Energy