Calculation of power dissipation in corps of onboard equipment of space vehicle in direct electrostatic discharge


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Abstract

Describes an example of the calculation of power dissipation in corps of onboard equipment of space vehicle in direct electrostatic discharge. The analysis of the obtained results in order to identify hazards thermal influence of electrostatic discharges on the temperature regime of onboard equipment of space vehicle.

About the authors

A. V. Kostin

Samara State Aerospace University

Author for correspondence.
Email: kipres@ssau.ru

Postgraduate student

Russian Federation

References

  1. Kostin AV Piganov MN The calculation of interference in the circuits onboard equipment spacecraft caused by electrostatic discharges / (Proceedings of the Samara Scientific Center of the Russian Academy of Sciences. 2012.T.14. № 4 (5). P. 1376-1379.
  2. (In Russ.)
  3. Jaworski B.F., Detlaf A.A. Handbook of physics. Nauka, 1964.-512.
  4. Sokolov A.B. Ensuring stability of onboard equipment space vehicles to the effects of electro-static discharge. Thesis for the degree of Doctor of Technical Sciences. Moscow: MIEM 2009.
  5. Kostin A.V. Analysis methods of protection board equipment cosmic devices against electrostatic discharge factors / Bulletin of the Samara State Aerospace University vennogo-2011. № 7 (31). Р. 107-112. (In Russ.)
  6. Bessonov L.A. Theory of Electrical Engineering. Electromagnetic field. Textbook for electro-technical., Energy., Priborostroit. specials. uni-versities. 8th ed., Rev. and add. M.: Higher. scl., 1986. 236.
  7. Gonorovsky I.S. Radiotekhnical circuits and signals: A Textbook for wu-call. 4th ed., Rev. and add. M.: Radio and Communications, 1986. 512.

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