DEVELOPMENT OF COMPOSITE STRUCTURAL MATERIALS FOR SPACE VEHICLE APPLICATIONS.

Abstract

The concept of utilizing the extremely high strength of filamentary crystals (whiskers) for reinforcing metals is presented. Structural considerations of filament reinforcement and the problems of attaining the full reinforcing capabilities of whiskers are now discussed. An example is given for predicting the strengths of a composite consisting of a columbium alloy (F-48) reinforced with sapphire (Al2O3) whiskers. Such whiskers retain a considerable portion of their strength at elevated temperatures, e.g., tensile strengths of 150,000 psi at 3570 F. Calculations showed that reinforcing F-48 alloy with 50% Al2O3 whiskers could improve the strength-to-density ratio more than four-fold over a 3000 F temperature range. The preliminary results of an experimental program concerned with the development of composites of aluminum reinforced with Al2O3 whiskers and ZrO2 fibers are discussed. It is concluded that the crux of utilizing the full reinforcing potential of whiskers lies in the careful orientation, wetting, and bonding of the whiskers in the metal phase. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1961
Accession Number
AD0607653

Entities

People

  • Willard H. Sutton

Organizations

  • General Electric

Tags

DTIC Thesaurus Topics

  • Aluminum
  • Chemical Compounds
  • Composite Materials
  • Filaments
  • Inorganic Chemicals
  • Materials
  • Metals
  • Minerals
  • Niobium
  • Orientation (Direction)
  • Sapphire
  • Spacecraft
  • Synthetic Materials
  • Tensile Strength
  • Vehicles

Fields of Study

  • Materials science

Readers

  • Materials Science and Engineering.
  • Reinforced Composite Materials
  • Theoretical Analysis.

Technology Areas

  • Space