HIGH VISCOSITY THERMAL PROTECTION MATERIALS.

Abstract

Processes were developed for hot pressing a 68.5% tungsten-31.5% silica composition to over 97% of the calculated theoretical density. Hot pressing characteristics changed when crystalline silica was substituted for vitreous silica. Grinding and hot pressing methods were studied for fabricating test nozzles for the NOL oxyhydrogen rocket motor. Gases entrapped during hot pressing are expected to be a factor in ablation performance. Vacuum-argon sintering of the silica-tungsten mixture was studied and photomicrographs revealed a structure similar to that of the Bjorksten Laboratory specimens but different from that of hot pressed material. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 16, 1966
Accession Number
AD0646616

Entities

People

  • D. M. Caum
  • Roger E. Wilson

Organizations

  • Naval Ordnance Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Ablation
  • Buildings And Structures
  • Hot Pressing
  • Materials
  • Materials Processing
  • Mechanical Properties
  • Mechanical Working
  • Research Facilities
  • Rocket Engines
  • Rockets
  • Sintering
  • Tungsten
  • Viscosity

Fields of Study

  • Materials science

Readers

  • Powder metallurgy of Titanium alloys.
  • Rocket Propulsion.