STUDY OF THE EFFECTS OF ENVIRONMENTAL CONDITIONS ON THE BREAKDOWN OF ANTENNAS AT LOW PRESSURES ON A SUPERSONIC VEHICLE

Abstract

The breakdown characteristics of antennas under supersonic flight conditions at altitudes up to 80 miles were investigated. Three Nike-Cajun rockets were instrumented and fired from Eglin Gulf Test range. Significant results were obtained only one firing. Details of the instrunentation are given, as well as a discussion of the data obta%ned. Data are given on the fiF power required to initiate and extinguish breakdown, surface temperatures, and pressure on the surface of the conical nose. A comparison of breakdown data with previously obtained laboratory data and with the theory of breakdown phenomena reveals discrepancies which remain unresolved due to the limited quantity of flight data available for analysis.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1961
Accession Number
AD0267163

Entities

People

  • J. B. Chown
  • M. G. Keenan

Organizations

  • SRI International

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Altitude
  • Detectors
  • Electric Fields
  • Electron Density
  • Energy Transfer
  • Frequency
  • Instrumentation
  • Mach Number
  • Measurement
  • New York
  • Power Supplies
  • Radar
  • Repetition Rate
  • Supersonic Flight
  • Surface Temperature
  • Telemetry Equipment

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Oceanography.
  • Plasma Physics.

Technology Areas

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