• DocumentCode
    3711230
  • Title

    Solar electric propulsion for future NASA missions

  • Author

    Geoffrey A. Landis;Steven R. Oleson;Carolyn R. Mercer

  • Author_Institution
    NASA Glenn Research Center, 21000 Brookpark Road, Cleveland OH 44135, United States of America
  • fYear
    2015
  • fDate
    6/1/2015 12:00:00 AM
  • Firstpage
    1
  • Lastpage
    4
  • Abstract
    Use of high-power solar arrays, at power levels up to a megawatt, have been proposed for a solar-electric propulsion (SEP) missions, using photovoltaic arrays to provide energy to high-power xenon-fueled engines. One of the proposed demonstrations of high-power SEP technology is a mission to rendezvous with an asteroid and move it into lunar orbit for human exploration, the Asteroid Redirect mission. NASA´s Solar Electric Propulsion project is dedicated to developing critical technologies to enable trips destinations such as Mars or asteroids. NASA needs to reduce the cost of these ambitious exploration missions. High power and high efficiency SEP systems will require much less propellant to meet those requirements.
  • Keywords
    "Propulsion","Space vehicles","Mars","NASA","Moon","Orbits"
  • Publisher
    ieee
  • Conference_Titel
    Photovoltaic Specialist Conference (PVSC), 2015 IEEE 42nd
  • Type

    conf

  • DOI
    10.1109/PVSC.2015.7355948
  • Filename
    7355948