A magnetic nozzle having a converging/diverging contour shape that converts the thermal energy of a propellant into directed kinetic energy, but uses magnetic fields instead of a physical boundary to direct the flow of particles.


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    Title :

    СХОДЯЩЕЕСЯ/РАСХОДЯЩЕЕСЯ МАГНИТНОЕ СОПЛО


    Publication date :

    2017-10-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS