DEVELOPMENT AND UTILIZATION OF OPTIMUM TECHNIQUES FOR THE FABRICATION OF TITANIUM BORONITRIDE ROCKET NOZZLES.

Abstract

Various test specimens and rocket nozzle inserts were produced of various throat diameters from a material composed principally of titanium diboride, titanium nitride and boron nitride. The scope of this project is to develop optimum techniques for fabricating sound, dense, crackfree specimens and rocket nozzle inserts in specified sizes of the material system - Titanium, Boron, Nitrogen. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1963
Accession Number
AD0429467

Entities

People

  • R. Strickman

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Ceramic Materials
  • Diameters
  • Fabrication
  • Gas Turbine Nozzles
  • Materials
  • Nitrogen
  • Nozzles
  • Rocket Nozzles
  • Rockets
  • Titanium

Fields of Study

  • Physics

Readers

  • Metallurgy
  • Rocket Propulsion.
  • Surface Engineering/Surface Coating Technology.