Temperature Measurements of 30-MM Regenerative Liquid Propellant Gun (RLPG) Firings

Abstract

Gas phase temperature measurements were made during 30-mm regenerative liquid propellant gun (RLPG) firings with an invasive spectroscopic technique developed at the Ernst Mach Institute. The technique was based on measuring the brightness temperature of the combustion gas with an optical probe emission gage. Planck's distribution of blackbody emission was used as the basis for calibrating the emission gage, thus providing a theoretical basis for extrapolating the response of the gage beyond the maximum calibration temperature. The propellant used in the test was LGP 1845, which has an adiabatic flame temperature of 2,592 K. The spectroscopic technique, calibration procedure, and experimental results are discussed. The results yielded maximum temperatures between 2,200 K and 2,450 K, or 5 to 15 percent below the adiabatic flame temperature. The results show fair qualitative agreement with a lumped parameter computer model.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1991
Accession Number
ADA233720

Entities

People

  • John D. Knapton
  • Nathan E. Boyer
  • Phillip Reeves
  • Terence P. Coffee

Organizations

  • Ballistic Research Laboratory

Tags

Communities of Interest

  • Energy and Power Technologies
  • Materials and Manufacturing Processes
  • Weapons Technologies

DTIC Thesaurus Topics

  • Adiabatic Flames
  • Agreements
  • Brightness
  • Calibration
  • Chambers
  • Combustion
  • Combustion Chambers
  • Commerce
  • Emission
  • Flames
  • Gun Propellants
  • Guns
  • Liquid Propellant Guns
  • Liquid Propellants
  • Measurement
  • Pressure Measurement
  • Propellants

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.
  • Thermal Physics or Thermal Science.
  • ballistics.