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 in:High temperature 2020-03, Vol.58 (2), p.162-165
Main Authors: Kotel’nikov, V. A., Kotel’nikov, M. V., Kassin, D. V.
Format: Article
Language:English
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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Description
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