Quantitative Evaluation of the Impulse-bit Generated in a Magnetic Thrust Chamber

DOI

Description

<p>A magnetic thrust chamber is a component of a propulsion system which obtain thrust from a plasma in using a magnetic field. A laser fusion rocket has been assumed to use this system and will be used for interplanetary flight. To realize this rocket, we need to investigate the thrust performance of the magnetic thrust chamber. Previous work has investigated the plasma behaviour and thrust using simulations and experiments. However, quantitative comparison has not been much. In this work, we quantitatively compared computational and experimental results of plasma behaviour and performance. It was observed that the impulse bit increases as the magnetic field strength however, results from the experiment were approximately 3 times larger than that of simulation.</p>

Journal

Keywords

Details 詳細情報について

  • CRID
    1390576844714555776
  • DOI
    10.57350/jesa.4
  • ISSN
    27581802
  • Text Lang
    en
  • Data Source
    • JaLC
  • Abstract License Flag
    Allowed

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