• DocumentCode
    3515604
  • Title

    In-Space Propulsion Electric Propulsion Technologies Mission Benefits

  • Author

    Dankanich, John W.

  • Author_Institution
    Gray Res. Inc., Cleveland, OH
  • fYear
    2008
  • fDate
    1-8 March 2008
  • Firstpage
    1
  • Lastpage
    7
  • Abstract
    The primary source of electric propulsion development within NASA is the In-Space Propulsion Technology (ISPT) Project at the NASA Glenn Research Center under the management of the Science Mission Directorate. The electric propulsion (EP) technology area´s objective is to develop near and mid-term EP technology that enhances or enables mission capture while minimizing risk and cost to the end user. Major activities include developing NASA´s evolutionary xenon thruster (NEXT) and a long life high voltage hall accelerator (HiVHAC). Lower level investments include advanced feed system development, evaluating life qualification standards, and evaluating the applicability of commercially available systems to NASA science missions. Mission benefits of investment technologies for Discovery, New Frontiers, and Flagship mission are presented.
  • Keywords
    aerospace propulsion; electric propulsion; space vehicles; Glenn Research Center; NASA; Science Mission Directorate; electric propulsion; evolutionary xenon thruster; high voltage hall accelerator; in-space propulsion technologies; life qualification standards; mission benefits; Costs; Investments; NASA; Project management; Propulsion; Research and development management; Space technology; Technology management; Voltage; Xenon;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2008 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-1487-1
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2008.4526548
  • Filename
    4526548