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

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

Russian Federation

Doctor of Technical Science

Professor of the Department of Radio Engineering and Medical Diagnostic Systems

V. V. Bragin

Samara State Aerospace University

Email: bragin_vv@inbox.ru

Russian Federation

Postgraduate Student

R. A. Pomelnikov

Samara State Aerospace University

Email: r_cosmos@mail.ru

Russian Federation

Junior Research Associate

V. L. Balakin

Samara State Aerospace University

Email: balakin@ssau.ru

Russian Federation

Doctor of Technical Science

Professor of the Department of Space Engineering

References

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