Alleviation of the Plasma Boundary Layer by Chemical Injection,

Abstract

Work performed on the transmission and radiation characteristics of antennas on the surface of a plasma-covered wind tunnel model is reported. The model used is a blunted cone-cylinder operated in a supersonic wind tunnel at M = 4, To = 80 to 100 F and P(o) = 1.2 to 3 psi. The plasma sheath was obtained by injecting nitrogen plasma from a DC arc jet located in the model nose. A new chemical injection system was used to inject a number of halogenated hydrocarbons into the plasma layer. It was found that nearly complete restoration of free space antenna impedance and transmitted power could be achieved from 25 mw S-Band signals at 50 percent or less additive mass fraction. Data from electrostatic probes is presented which indicates that the mechanism of alleviation is electron attachment to form heavy negative species. Teflon and carbon phenolic ablative plasmas were also studied and the effects of these ablative materials on the plasma sheath are presented. The effect of ultrasonic energy on small fluid jets was also studied, as was the penetration of these jets into the wind stream. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1970
Accession Number
AD0718976

Entities

People

  • Charles W. Haldeman
  • James P. Mcguirk

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Ablative Materials
  • Boundary Layer
  • Electrostatic Probes
  • Halogenated Hydrocarbons
  • Hydrocarbons
  • Layers
  • Materials
  • Models
  • Payload
  • Plasma Sheaths
  • Radiation
  • Supersonic Wind Tunnels
  • Wind Tunnel Models
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Propulsion Engineering.
  • Electromagnetic Wave Scattering and Antenna Radiation Engineering

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow
  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster