Experimental and Theoretical Studies of Laser Propulsion Phenomenology.

Abstract

This report summarizes progress on a research program carried out to investigate and define physical process important to the operation of pulsed and CW laser-heated thrusters. The work performed in this first year effort was divided into three tasks: (1) experimental measurements and quantum kinetic model calculations of the thresholds for laser-induced gas breakdown at visible and near UV wavelengths, (2) preliminary calculations of the spectral/radiant emissions from high temperature (T = 10,000 to 40,000 K), high pressure (P approx. 1 to 100 atm) plasmas of hydrogen and nitrogen, and (3) experimental measurements of the high temperature absorption properties of potential molecular seedants for a CW laser-heated thruster operating at lambda approx. 10 microns. The molecular absorption measurements were performed using a low power, line-tuneable C02 probe laser and a shock tube heating apparatus. (Author)

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1984
Accession Number
ADA140995

Entities

People

  • D. Ham
  • David M. Rosen
  • G. Weyl
  • N. Kemp

Organizations

  • Physical Sciences (United States)

Tags

Communities of Interest

  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Absorption
  • Emission
  • Gas Breakdown
  • High Pressure
  • High Temperature
  • Hydrogen
  • Lasers
  • Measurement
  • Nitrogen
  • Pressure Measurement
  • Shock Tubes
  • Thrusters
  • Tubes

Fields of Study

  • Physics

Readers

  • Pulsed Power and Plasma Physics.

Technology Areas

  • Directed Energy
  • Directed Energy - Lasers
  • Quantum Computing
  • Space
  • Space - Hall-Effect Thruster