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There are several significant problems associated with the electrification of the nozzle walls due to the presence of charged particles in the working fluid flow. The detailed study of these problems and the determination of effective ways to eliminate them is part of the research presented by the authors of this work, which is devoted to the calculation and evaluation of the electric field strength in rocket engines on both solid and liquid fuels.

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Calculation of Electric Field Strength in Supersonic Plasma Flow of Combustion Products of Rocket Engines on Solid and Liquid Fuels

  • 会议论文

  • 发表日期：

    2026年

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  • Valery V. Onufriev,
  • Roman M. Kramarenko

摘要

There are several significant problems associated with the electrification of the nozzle walls due to the presence of charged particles in the working fluid flow. The detailed study of these problems and the determination of effective ways to eliminate them is part of the research presented by the authors of this work, which is devoted to the calculation and evaluation of the electric field strength in rocket engines on both solid and liquid fuels.