FLAME TEMPERATURE MEASUREMENT OF METALIZED PROPELLANT

Abstract

The spectral comparison method has been developed for the measurement of temperatures of both the gas and condensed phase in a flame. This method utilizes measurements of spectrum line emission from the gas and continuum emission from particle cloud to allow determination of the temperature of both phases. The method accounts for the effect of scattering by the particle cloud through measurements of effective particle size and number density used in conjunction with the Mie theory. The measurement precision for this method for a clean gas was determined from measurements on a H2/O2 flame; the resulting standard deviation in gas temperature was 16 K. With particles of alumina introduced into the flame, the standard deviation in gas temperature was increased to 40.8 K. For the particle temperature the standard deviation was 140 K, a relatively high value because of the uncertainty in the refractive index of molten alumina. The first spectral line of the sodium doublet (0.589 micron) was assessed to be a good indicator of the gas temperature in flames. This was determined by a comparison to the lithium line at 0.6708 micron which is associated with an electron transition of longer radiative lifetime.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jun 27, 1966
Accession Number
AD0375897

Entities

People

  • Jim M. Adams
  • Steve E. Colucci

Organizations

  • Aerojet Rocketdyne Holdings

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aluminum Oxides
  • Combustion
  • Lasers
  • Light Scattering
  • Light Sources
  • Materials
  • Materials Processing
  • Materials Science
  • Measurement
  • Optics
  • Particle Size
  • Propellant Grains
  • Refractive Index
  • Rocket Engines
  • Scattering
  • Spectra
  • Spectral Lines

Fields of Study

  • Physics

Readers

  • Atmospheric Remote Sensing.
  • Quantum spin resonance or Electron Paramagnetic Resonance spectroscopy.
  • Rocket Propulsion.

Technology Areas

  • Microelectronics