NASAs Evolutionary Xenon Thruster (NEXT) project is developing next generation ion propulsion technologies to enhance the performance and lower the costs of future NASA space science missions. This is being accomplished by producing Engineering Model (EM) and Prototype Model (PM) components, validating these via qualification-level and integrated system testing, and preparing the transition of NEXT technologies to flight system development. This presentation is a follow-up to the NEXT project overviews presented in 2009-2010. It reviews the status of the NEXT project, presents the current system performance characteristics, and describes planned activities in continuing the transition of NEXT technology to a first flight. In 2013 a voluntary decision was made to terminate the long duration test of the NEXT thruster, given the thruster design has exceeded all expectations by accumulating over 50,000 hours of operation to demonstrate around 900 kg of xenon throughput. Besides its promise for upcoming NASA science missions, NEXT has excellent potential for future commercial and international spacecraft applications.


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    Titel :

    Recent Development Activities and Future Mission Applications of NASA's Evolutionary Xenon Thruster (NEXT)


    Beteiligte:
    M. J. Patterson (Autor:in) / E. J. Pencil (Autor:in)

    Erscheinungsdatum :

    2014


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Mission Advantages of NEXT: NASA's Evolutionary Xenon Thruster

    Oleson, Steven / Gefert, Leon / Sims, Jon et al. | AIAA | 2002


    Mission Advantages of NEXT: NASA's Evolutionary Xenon Thruster

    S. Oleson / L. Gefert / S. Benson et al. | NTIS | 2002


    Mission Advantages of NEXT: Nasa's Evolutionary Xenon Thruster

    Oleson, Steven / Gefert, Leon / Benson, Scott et al. | NTRS | 2002


    Deep Space Mission Applications for NEXT: NASA's Evolutionary Xenon Thruster

    Oh, David / Benson, Scott / Witzberger, Kevin et al. | AIAA | 2004