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  1. No Access

    Article

    Experimental study of energy balance for an electro-rocket thruster with an anode layer and power up to 1000 W

    Experimental results and a procedure for determining the total energy balance for single-stage thrusters with azimuth electron drift are presented. A single-stage thruster with an anode layer (TAL) with power ...

    D. N. Alekseev, M. K. Marakhtanov, A. V. Pil’nikov, V. V. Sinyavskii in Thermal Engineering (2014)

  2. No Access

    Article

    Investigation of the ion beam of a plasma accelerator with azimuthal drift of electrons by an optical method

    D. N. Alekseev, A. B. Vagapov, M. K. Marakhtanov… in Journal of Applied Spectroscopy (1992)