Plane high-speed particle transducer

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Abstract

The paper presents the solution to the problem of constructing a mathematical model of a high-speed particle ionisation transducer of a plane design. The results of experiments with the plane transducer carried out with the help of a pulsing laser are discussed.

About the authors

M V. Izyumov

Samara Space Rocket Centre “TsSKB-Progress”

Author for correspondence.
Email: izumov_mike.csdb@mail.ru
Russian Federation

N. D. Syomkin

Samara State Aerospace University

Email: semkin@ssau.ru
Russian Federation

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Copyright (c) 2015 VESTNIK of the Samara State Aerospace University

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