TUNGSTEN AND ROCKET MOTORS

Abstract

Erosion experiments were made on small tungsten rods with Al2O3 in the plasma flame at temperatures near the melting point of W. The specimens, 5/32-inch-diameter tungsten Heli-arc electrodes approximately 3-1/2 inches long (2% thorium, close to 100% theoretical densi y), were positioned coaxially with the plasma flame and the tip temperature was measured with an optical pyrometer which had been calibrated for experimental conditions at the melting point of tungsten. Erosion parameters measured were the change in specimen length, and the weight loss or gain. Al2O3 alone does not cause significant erosion of W. A mathematical calculation of the thermal stresses on the outer ring fiber is given. It is therefore desirable to be able accurately to measure or calculate the thermal stress on the outer ring fiber. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 07, 1961
Accession Number
AD0266664

Entities

People

  • Gerald M. Gordon

Organizations

  • SRI International

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Body Weight
  • Diameters
  • Electrodes
  • Melting
  • Melting Point
  • Optical Pyrometers
  • Pyrometers
  • Rocket Engines
  • Rockets
  • Stresses
  • Thermal Stresses
  • Tungsten

Fields of Study

  • Physics

Readers

  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Surface Engineering/Surface Coating Technology.
  • Thermal Physics or Thermal Science.