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Probe Measurements on Board a Hypersonic Aircraft

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Abstract

The features of probe measurements on a hypersonic aircraft, the design of the probe block and its location on a hypersonic aircraft, and the processing technique of the obtained current-voltage characteristics are discussed. Original processing techniques are proposed, and some results of probe measurements, covering both the plasma parameters in the combustion products of a liquid propellant rocket engine and the parameters of the plasma arising at supersonic speeds near the hypersonic aircraft wall, are presented.

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Authors and Affiliations

  1. Moscow Aviation Institute, Moscow, Russia

    V. A. Kotel’nikov, M. V. Kotel’nikov & D. V. Kassin

  2. Blagonravov Institute of Mechanical Engineering, Russian Academy of Sciences, Moscow, Russia

    V. A. Kotel’nikov, M. V. Kotel’nikov & D. V. Kassin

Authors
  1. V. A. Kotel’nikov
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  2. M. V. Kotel’nikov
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  3. D. V. Kassin
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Corresponding authors

Correspondence to M. V. Kotel’nikov or D. V. Kassin.

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Translated by L. Mosina

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Kotel’nikov, V.A., Kotel’nikov, M.V. & Kassin, D.V. Probe Measurements on Board a Hypersonic Aircraft. High Temp 58, 162–165 (2020). https://doi.org/10.1134/S0018151X2002011X

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  • DOI: https://doi.org/10.1134/S0018151X2002011X

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