Applicability of Electric Propulsion for Future Military Satellites

Abstract

The feasibility of using electric propulsion subsystems to perform conventional propulsion functions in mission areas of Air Force interest is investigated. Consideration is given to using electric propulsion either alone or in conjunction with conventional propulsion subsystems. In each case, the results are compared with the conventional propulsion subsystem that otherwise would be used. The analysis identifies some areas wherein the application of electric propulsion would result in substantial cost savings, but the study also indicates other areas in which the applications of electric propulsion is not cost effective for the missions under consideration in this study.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1973
Accession Number
AD0769521

Entities

People

  • Calvin W. Thomas
  • Wendell M. Adamson

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Apogees
  • Artificial Satellites
  • Computer Programs
  • Cost Estimates
  • Earth Orbits
  • Electric Power
  • Electric Propulsion
  • Equatorial Orbits
  • Geosynchronous Satellites
  • Jet Propulsion
  • Plastic Explosives
  • Propulsion Systems
  • Rocket Propulsion
  • Solar Panels
  • Space Transportation
  • Spacecraft
  • Spacecraft Orbits

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Life Cycle Cost Analysis

Technology Areas

  • Space
  • Space - Hall-Effect Thruster
  • Space - Satellites