Radiation Augmented Propulsion Feasibility.

Abstract

Gas phase absorption of solar radiation has been suggested as an energy source to power space propulsion systems. The absorbing gas could be an expendable propellant or could be used in a closed cycle, exchanging heat with an expendable propellant. This study was conducted in order to develop basic data and understanding useful for the evaluation of such a system with the absorbing gas being a halogen or an interhalogen. Experiments and analysis were conducted to characterize the absorption of ultraviolet and visible radiation and subsequent energy release in chlorine gas, iodine monochloride vapor, and mixtures of hydrogen gas and chlorine gas. Xenon flashlamps were used to provide the radiation. Measurements included lamp electrical and optical characteristics, light energy absorbed, pressure rise in the closed reactor and reactants remaining after the reaction. Analysis included detailed kinetic modeling of the single shot experiments.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1985
Accession Number
ADA163983

Entities

People

  • J. Blauer
  • J. R. Hall
  • R. I. Wagner
  • S. C. Hurlock
  • V. Quan

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Chemical Kinetics
  • Chemical Reaction Properties
  • Chemical Reactions
  • Chemistry
  • Computer Programs
  • Dielectric Gases
  • Dissociation
  • Energy
  • Energy Transfer
  • Numerical Analysis
  • Physical Chemistry
  • Physics
  • Physics Laboratories
  • Pressure Measurement
  • Propulsion Systems
  • Solar Radiation
  • Space Propulsion

Fields of Study

  • Physics

Readers

  • Molecular Photonics/Laser Physics
  • Nuclear and Radiation Engineering.
  • ballistics.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster