Probe Measurements on Board a Hypersonic Aircraft

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 mea...

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Bibliographic Details
Published inHigh temperature Vol. 58; no. 2; pp. 162 - 165
Main Authors Kotel’nikov, V. A., Kotel’nikov, M. V., Kassin, D. V.
Format Journal Article
LanguageEnglish
Published Moscow Pleiades Publishing 01.03.2020
Springer Nature B.V
Subjects
Aircraft
Aircraft design
Aircraft rockets
Atoms and Molecules in Strong Fields
Classical and Continuum Physics
Combustion products
Current voltage characteristics
Engine blocks
Hypersonic aircraft
Industrial Chemistry/Chemical Engineering
Laser Matter Interaction
Liquid propellant rocket engines
Liquid propellants
Materials Science
Parameters
Physical Chemistry
Physics
Physics and Astronomy
Plasma Investigations
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Summary: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.
ISSN:0018-151X
1608-3156
DOI:10.1134/S0018151X2002011X