ADVANCED COMPOSITE CARBIDE NOZZLES.

Abstract

The purpose of this program is to develop thermal-shock-resistant composite carbides that can be reliably used with high-flame-temperature solid rocket propellants. During the first quarter, composition and fabrication variables necessary to optimize a tantalum/hafnium monocarbide microcomposite structure were investigated. A hot-press fabrication technique was used. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1966
Accession Number
AD0800260

Entities

People

  • L. M. Swope
  • R. P. Radtke

Organizations

  • Aerojet Rocketdyne Holdings

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Composite Materials
  • Energetic Materials
  • Fabrication
  • Material Forming Processes
  • Materials
  • Materials Processing
  • Propellants
  • Rocket Propellants
  • Shock
  • Solid Rocket Propellants
  • Tantalum
  • Thermal Shock

Readers

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