HIGH TEMPERATURE RESISTANT MATERIALS FOR MISSILE PROPULSION SYSTEMS

Abstract

Oxy-acetylene torch test studies on a series of experimental phenolic resins are described along with those conducted on a number of commercial ablation type materials. A phenolic-polyamide copolymer was found to be the most effective for insulation effectiveness. The potential of silicone rubber as the matrix for an effective elastomeric insulator was demonstrated.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jan 30, 1963
Accession Number
AD0408362

Entities

People

  • F. J. Koubek

Organizations

  • Naval Ordnance Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Ablation
  • Chemistry
  • Composite Materials
  • Corporations
  • Guided Missiles
  • Heat Flux
  • Insulation
  • Jet Propulsion
  • Materials
  • Materials Science
  • Munitions
  • Ordnance Laboratories
  • Propulsion Systems
  • Rockets
  • Standardization
  • Standards
  • Test Methods

Fields of Study

  • Physics

Readers

  • Polymer Science and Engineering.
  • Reinforced Composite Materials

Technology Areas

  • Microelectronics