Hall effect thrusters for small-sized spacecrafts
... application as a part of electric propulsion systems (EPS) for small-sized spacecrafts are presented. Based on the analysis of main parameters and characteristics, the most prospective scheme of the EP design has been selected.
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Патент
РФ
№
2191289,
кл
. 6 H 05H 1/54, F 03H 1/00.
Gopanchuk V. V., Potapenko M. Yu.
Gas Breakdown, Hall or Stationary Plasma Thruster, Electrical Insulator.
131-137