A Breakdown Surface Model for Thermal Backscattering from the Exhaust Plume of a Space-Based HF Laser.

Abstract

The purpose of this report is to present a breakdown surface model for evaluating thermal backscattering flow from the supersonic exhaust plume of a gaseous mixture of H, HF, H2, DF and He. Fluxes of these species are considered separately. The model is carefully analyzed and is shown to overestimate the flux. Actual flux levels of the heavy corrosive molecules (HD, DF) have been found to be exceedingly low. It is concluded that the contribution of thermal backscattering to contaminating flux of HF and DF can be neglected.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1986
Accession Number
ADA171616

Entities

People

  • Joseph Falcovitz

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Backscattering
  • Boundary Layer
  • Chemical Lasers
  • Computers
  • Contractors
  • Equations
  • Exhaust Plumes
  • Flow Fields
  • Hydrogen Fluoride Lasers
  • Lasers
  • Mach Number
  • Mainframe Computers
  • Molecular Weight
  • Molecules
  • Plumes
  • Space Based
  • Stagnation Temperature

Fields of Study

  • Physics

Readers

  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Radar Systems Engineering.
  • Rocket Propulsion.

Technology Areas

  • Directed Energy
  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Space
  • Space - Hall-Effect Thruster