A fundamental study of a newly developed rectangular pulsed laser‐electromagnetic hybrid thruster was conducted. Laser‐ablation plasma in the thruster was induced through laser beam irradiation onto a solid target and accelerated by electrical means instead of direct acceleration only by using a laser beam. The performance of the thrusters was evaluated by measuring the ablated mass per pulse and impulse bit. As results, significantly high specific impulses up to 7,200 s were obtained at charge energies of 8.6 J. Moreover, from the Faraday cup measurement, it was confirmed that the speed of ions was accelerated with addition of electric energy.


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    Titel :

    Acceleration Mechanism Of Pulsed Laser‐Electromagnetic Hybrid Thruster


    Beteiligte:
    Horisawa, Hideyuki (Autor:in) / Mashima, Yuki (Autor:in) / Yamada, Osamu (Autor:in) / Eckel, Hans‐Albert (Herausgeber:in) / Scharring, Stefan (Herausgeber:in)

    Kongress:

    BEAMED ENERGY PROPULSION: Seventh International Symposium ; 2011 ; Ludwigsburg, (Germany)


    Erschienen in:

    AIP Conference Proceedings ; 1402 , 1 ; 391-401


    Erscheinungsdatum :

    10.11.2011


    Format / Umfang :

    11 pages





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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