HIGH TEMPERATURE RESISTANT MATERIALS FOR MISSILE PROPULSION SYSTEMS

Abstract

Steady state ablation was reached in oxy-acetylene burner tests on extra long specimens of phenolic asbestos. Also tested and analyzed were two densities of foamed silica. Calculation of alpha vs. temperature from experimental data was programmed for a digital computer. A detailed study of the NOL transient calorimeter was made. Generally, the existence of a linear temperature rise on the back face is sufficient evidence that errors are negligible.

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Document Details

Document Type
Technical Report
Publication Date
Oct 09, 1967
Accession Number
AD0662679

Entities

People

  • Bruce Hartmann
  • F. J. Koubek

Organizations

  • Naval Ordnance Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Ablative Materials
  • Accuracy
  • Blast Tubes
  • Calorimeters
  • Digital Computers
  • Experimental Data
  • Fluid Mechanics
  • High Temperature
  • Isotherms
  • Liquid Propellants
  • Materials Testing
  • Measurement
  • Nomenclature
  • Ordnance Laboratories
  • Standards
  • Test Methods
  • Thermal Diffusivity

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Computer Science/Computer Engineering/Data Science/Digital Signal Processing.
  • Polymer Science and Engineering.