GAS FLOW, EMITTANCE, AND ION CURRENT CAPABILITIES OF POROUS TUNGSTEN

Abstract

Analysis of Cs ion current and propellant utilization capabilities of porous W, based on a simple model of a porous structure, indicates that pore sizes of 1 micron and less would be desirable. bGas flow measurements indicated that some difficulty might be experienced in operating smaller particle size porous W structures at the required surface temperature for high current density because of the possible sintering of the W. Experimental gas flow measurements through porous W disks made from 1-, 10-, and 20-micron powder are presented. Sintering temperatures above 1500 K affected the permeability of the 1-micron-pore material. This temperature range is a desired operating range of the Cs-W system for ion rocket applications. Emissivity measurements on these same materials yielded an average spectral emittance of about 0.8 at a wavelength of 0.65 micron. Total radiation measurements gave emittance values in the range of 0.31 to 0.68. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1961
Accession Number
AD0262047

Entities

People

  • Lawrence W. Kreps
  • Thaine W. Reynolds

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Current Density
  • Emissivity
  • Emittance
  • Flow
  • Gas Flow
  • Hydrodynamics
  • Materials
  • Measurement
  • Particle Size
  • Particles
  • Propellants
  • Sintering
  • Spectral Emittance
  • Surface Temperature

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Pulsed Power and Plasma Physics.
  • Surface Engineering/Surface Coating Technology.