Comparison of chemical and electrical propulsion systems for interplanetary missions and for satellite orientation shows advantages of latter consisting of accelerator, which produces thrust, propellant storage tank, and nuclear reactor-electric generator which supplies energy; electrical energy conversion methods; work at Boeing Airplane Co on confined parallel rail pulsed plasma accelerator main objective of which was examination of its efficiency, thrust level, and operating lifetime.


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    Titel :

    Pulsed plasma accelerator for space propulsion


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Maes, M.E. (Autor:in)

    Kongress:

    SAE Meeting ; 1961 Electric propulsion



    Erscheinungsdatum :

    1961


    Format / Umfang :

    12 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    The Pulsed Plasma Accelerator for Space Propulsion

    Maes, Michel E. | SAE Technical Papers | 1961


    Laser plasma accelerator for space propulsion

    Horisawa, Hideyuki / Kimura, Itsuro | AIAA | 2001



    A Pulsed Laser-Electromagnetic Hybrid Accelerator for Space Propulsion Application

    Shinohara, T. / Horisawa, H. / Baba, M. et al. | British Library Conference Proceedings | 2010