Modeling of electrostatic discharge impact transmitting through spacecraft cabling
DOI: 10.21293/1818-0442-2020-23-2-103-107
DOI: 10.21293/1818-0442-2020-23-2-103-107
Abstract: The aim of this research was to detail the cabling model from solar array to electrical power convert equipment of the spacecraft in terms of electrostatic discharge impact transmitting. Detailed cabling model is the part of power-supply system model that will be used for electrostatic discharge impact on spacecraft on-board equipment analysis.
Keywords: spacecraft, power-supply system, electrostatic discharge, cabling, distributed parameter line
Authors and copyright holders:
—
For citation:
Kiselev P. V., Bukreev V. G., Gebgardt V. A. Modeling of electrostatic discharge impact transmitting through spacecraft cabling. Doklady Tomskogo gosudarstvennogo universiteta sistem upravleniya i radioelektroniki, 2020, vol. 23, no. 2, pp. 103–107. DOI: 10.21293/1818-0442-2020-23-2-103-107
Executive Secretary of the Editor’s Office
Editor’s Office: 40 Lenina Prospect, Tomsk, 634050, Russia
Phone / Fax: + 7 (3822) 701-582
Viktor N. Maslennikov
Executive Secretary of the Editor’s Office
Editor’s Office: 40 Lenina Prospect, Tomsk, 634050, Russia
Phone / Fax: + 7 (3822) 51-21-21 / 51-43-02