Modeling of electrostatic discharge impact transmitting through spacecraft cabling

Download article in PDF format

Authors: Kiselev P. V., Bukreev V. G., Gebgardt V. A.

Annotation: 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: distributed parameter line, cabling, electrostatic discharge, power-supply system, spacecraft

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

  vnmas@tusur.ru

Subscription for updates