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Probe Measurements on Board a Hypersonic Aircraft
High Temperature ( IF 1.0 ) Pub Date : 2020-06-29 , DOI: 10.1134/s0018151x2002011x V. A. Kotel’nikov , M. V. Kotel’nikov , D. V. Kassin
中文翻译:
高超音速飞机上的探头测量
更新日期:2020-06-29
High Temperature ( IF 1.0 ) Pub Date : 2020-06-29 , DOI: 10.1134/s0018151x2002011x V. A. Kotel’nikov , M. V. Kotel’nikov , D. V. Kassin
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:
高超音速飞机上的探头测量