Accession Number:

AD0647309

Title:

HIGH TEMPERATURE RESISTANT MATERIALS FOR MISSILE PROPULSION SYSTEMS.

Descriptive Note:

Summary rept., 30 Jun 65-30 Jun 66,

Corporate Author:

NAVAL ORDNANCE LAB WHITE OAK MD

Personal Author(s):

Report Date:

1966-12-27

Pagination or Media Count:

51.0

Abstract:

A temperature prediction program showed agreement to within 10 to 25 of experimental internal temperature for three ablators tested in the oxy-acetylene burner. However, if alpha effective thermal diffusivity is not obtained under steady-state ablation conditions, the agreement could be several hundred per cent in error. The alpha-rod test technique was found to be useful for ablators with widely varying properties. The NOL oxy-acetylene panel test was accepted and published as a tentative ASTM method. Author

Subject Categories:

  • Laminates and Composite Materials
  • Air Conditioning, Heating, Lighting and Ventilating
  • Test Facilities, Equipment and Methods
  • Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE