Study of conditions of electric breakdown in the flow part of electrical insulators of electric propulsion propellant supply systems :: IKBFU's united scientific journal editorial office

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The purpose of science is to transform all that exists into thought
Alexander Herzen

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Study of conditions of electric breakdown in the flow part of electrical insulators of electric propulsion propellant supply systems

Author Gopanchuk V. V., Potapenko M. Yu.
Pages 131-137
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Keywords Gas Breakdown, Hall or Stationary Plasma Thruster, Electrical Insulator.
Abstract (summary) The results of study of conditions of origination of electrical breakdown of gas in dielectric insulators of anode propellant (xenon) supply lines of prospective high-impulse increased-power electric thrusters intended for spacecraft orientation and stabilization are presented.
References

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2. Kozubsky K., Kudriavtsev S. et al. Study of Gas-Electrical Terminal in SPT // IEPC-99—062, 26th International Electric Propulsion Conference, Kitakyuschi, Japan, 1999.

3. Manzella David H., Jacobson David T. et al. High Voltage SPT Performance // AIAA-2001—3774, 37th Joint Propulsion Conference, Salt Lake City, Utah, 2001.

4. Патент РФ 2191289, кл. 6 H 05H 1/54, F 03H 1/00.


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