Development of Spacecraft Materials and Structures Fundamentals.

Abstract

Compacts of boron carbide powders with specific surface area = or > 8 sq m/g were sintered in argon at temperatures near 2200 C. Several of these powders were prepared by attrition milling of abrasive grade boron carbide. Densification to 95+% of theoretical denstiy could be obtained only with compositions that had appropriate amounts of excess carbon. The microstructures were fined grained and uniform but underwent abnormal grain growth above 2235 C accompanied by transgranular microcracking. This grain growth could be inhibited by increasing the carbon content. Mechanical damping capacity was measured by the free beam and cantilevered beam techniques on boron carbide and other materials. Methods to enhance the damping capacity in a beam structure were analyzed. The flexural strength of sintered boron carbide was evaluated and related to powder processing and sintering parameters. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1985
Accession Number
ADA161338

Entities

People

  • S. L. Dole
  • S. Prochazka

Organizations

  • General Electric

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Ceramic Materials
  • Chemical Synthesis
  • Chemistry
  • Diffraction
  • Flexural Strength
  • Grain Growth
  • Material Degradation Processes
  • Materials
  • Materials Laboratories
  • Materials Processing
  • Materials Science
  • Measurement
  • Mechanical Properties
  • Mechanical Working
  • Modulus Of Elasticity
  • Particle Size
  • Silicon Carbide

Readers

  • Plasma Physics.
  • Reinforced Composite Materials
  • Surface Engineering/Surface Coating Technology.

Technology Areas

  • Space