Accession Number:

AD0408362

Title:

HIGH TEMPERATURE RESISTANT MATERIALS FOR MISSILE PROPULSION SYSTEMS

Descriptive Note:

Summary rept., 30 June 1961-30 June 1962

Corporate Author:

NAVAL ORDNANCE LAB WHITE OAK MD

Personal Author(s):

Report Date:

1963-01-30

Pagination or Media Count:

51.0

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.

Subject Categories:

  • Solid Propellant Rocket Engines
  • Plastics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE