• DocumentCode
    1142535
  • Title

    Ion propulsion-a technology for improving the cost-effectiveness of large communications satellites

  • Author

    Fearn, D.G.

  • Author_Institution
    Space Dept., Defence Res. Agency, Farnborough, UK
  • Volume
    4
  • Issue
    3
  • fYear
    1992
  • fDate
    6/1/1992 12:00:00 AM
  • Firstpage
    153
  • Lastpage
    162
  • Abstract
    The overall launch mass of a communications satellite has a major influence on its economic performance. If this mass can be reduced substantially, the launch cost will be lower, or more revenue can be generated by carrying a larger payload or extending the operational lifetime. Since an ion propulsion system provides an exhaust velocity at least an order of magnitude higher than that of chemical thrusters, the propellant mass required for north-south station-keeping can be reduced by hundreds of kilogrammes, thereby gaining these benefits. This application of ion propulsion is discussed and quantified in the paper, for the Intelsat VII spacecraft and the UK-10 ion propulsion system
  • Keywords
    aerospace propulsion; artificial satellites; ion engines; satellite relay systems; Intelsat VII spacecraft; UK-10 ion propulsion system; economic performance; exhaust velocity; ion engines; large communications satellites; launch mass; north-south station-keeping; propellant mass;
  • fLanguage
    English
  • Journal_Title
    Electronics & Communication Engineering Journal
  • Publisher
    iet
  • ISSN
    0954-0695
  • Type

    jour

  • Filename
    149853