OPTIMIZATION OF FREQUENCIES FOR LOW-ALTITUDE SPACE COMMUNICATION,

Abstract

A simple technique is presented for obtaining the optimum frequencies for communication with a low-altitude satellite, no higher than 800 nautical miles. The output signal-to-noise ratio at the receiving station is expressed in terms of as many parameters as possible with their respective frequency dependence. The optimum frequency is obtained by a maximization process. In cases where the exact frequency behavior of the process is too complex, an approximate analytical expression is used. The parameters considered in this investigation are: the spatial electromagnetic path loss, the atmospheric absorption, the galactic noise temperature, the Faraday rotation effect, the antenna noise temperature, the receiver noise temperature, and the conversion efficiency of dc to rf power. The method yields optimum frequencies for the space-to-ground and the ground-to-space communication. For space-to-space communication the optimum frequency is selected from practical limitations. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1964
Accession Number
AD0463140

Entities

People

  • Gaspar R. Valenzuela

Organizations

  • Johns Hopkins University

Tags

Communities of Interest

  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Absorption
  • Altitude
  • Artificial Satellites
  • Atmospheric Attenuation
  • Conversion
  • Efficiency
  • Elevation
  • Frequency
  • Losses
  • Low Altitude
  • Nautical
  • Optimization
  • Power
  • Radio Frequency Power
  • Space Communications

Fields of Study

  • Engineering
  • Physics

Readers

  • Operations Research
  • Radar Systems Engineering.
  • Tactical Satellite Communications Systems Engineering.

Technology Areas

  • Space