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.

中文翻译：

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高超音速飞机上的探头测量

摘要

讨论了高超声速飞机上探针测量的特点，探针模块的设计及其在高超声速飞机上的位置以及获得的电流-电压特性的处理技术。提出了原始的处理技术，并给出了探针测量的一些结果，涵盖了液体推进火箭发动机燃烧产物中的等离子体参数和高超声速飞机壁附近以超音速产生的等离子体参数。