Method of calculating self-capacitance in planar structural elements of a spacecraft

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Abstract

The paper presents a methodology for calculating distribution of potentials based on the triangulation method of plane approximation, surface method and analytical determination of the matrix elements of Coulomb interaction. The results obtained demonstrate good agreement with the experiments on the electrization process in small spacecraft «AIST».

About the authors

N. D. Syomkin

Samara State Aerospace University

Author for correspondence.
Email: semkin@ssau.ru

Doctor of Technical Science

Professor of the Department of Radio Engineering and Medical Diagnostic Systems

Russian Federation

V. V. Bragin

Samara State Aerospace University

Email: bragin_vv@inbox.ru

Postgraduate Student

Russian Federation

R. A. Pomelnikov

Samara State Aerospace University

Email: r_cosmos@mail.ru

Junior Research Associate

Russian Federation

V. L. Balakin

Samara State Aerospace University

Email: balakin@ssau.ru

Doctor of Technical Science

Professor of the Department of Space Engineering

Russian Federation

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