Aerodynamic Studies of Antenna Breakdown, Part I.

Abstract

Work performed during 1967 and 1968 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, P sub o = 1.2 psia and T sub o = 100F. The plasma sheath is obtained by injecting nitrogen plasma from a DC arc jet located in the model nose. The effect of the plasma on X-band and S-band antennas located on the model surface was studied and it was found that the breakdown power and transmitted power of an X-band slot were greatly reduced by the plasma layer. The presence of the plasma layer was also found to increase the VSWR of an S-band slot from 1.2 to 20. Some development efforts associated with improvement of the arc jet are also presented. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1969
Accession Number
AD0855543

Entities

People

  • C. W. Haldeman
  • E. E. Covert
  • J.L. Sullivan
  • L. R. Boedeker

Organizations

  • Massachusetts Institute of Technology

Tags

DTIC Thesaurus Topics

  • Models
  • Nitrogen
  • Plasma Sheaths
  • Radiation
  • Supersonic Wind Tunnels
  • Wind Tunnel Models
  • Wind Tunnels
  • X Band

Fields of Study

  • Physics

Readers

  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Fluid Dynamics.
  • Plasma Physics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow