Microwave Rocket was operated with repetitive pulses. The microwave rocket model with forced breathing system was used. The pressure history in the thruster was measured and the thrust impulse was deduced. As a result, the impulse decreased at second pulse and impulses at latter pulses were constant. The dependence of the thrust performance on the partial filling rate of the thruster was compared to the thrust generation model based on the shock wave driven by microwave plasma. The experimental results showed good agreement to the predicted dependency.


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    Titel :

    An Experiment on Repetitive Pulse Operation of Microwave Rocket


    Beteiligte:
    Oda, Yasuhisa (Autor:in) / Shibata, Teppei (Autor:in) / Komurasaki, Kimiya (Autor:in) / Takahashi, Koji (Autor:in) / Kasugai, Atsushi (Autor:in) / Sakamoto, Keishi (Autor:in) / Pakhomov, Andrew V. (Herausgeber:in)

    Kongress:

    BEAMED ENERGY PROPULSION: Fifth International Symposium on Beamed Energy Propulsion ; 2007 ; Kailua‐Kona (Hawaii)


    Erschienen in:

    AIP Conference Proceedings ; 997 , 1 ; 453-459


    Erscheinungsdatum :

    28.04.2008


    Format / Umfang :

    7 pages





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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