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.
1. Potapenko M.Yu., Gopanchuk V. V. Characteristic Relationship between Dimensions and Parameters of a hybrid Plasma Thruster // IEPC-2011—042, 32nd International Electric Propulsion Conference. Wiesbaden, 2011.
2. Гопанчук В. В., Никулин Н. М., Потапенко ...
Study of conditions of electric breakdown in the flow part of electrical insulators of electric propulsion propellant supply systems
Manzella David H., Jacobson David T.
et al. High Voltage SPT Performance // AIAA-2001—3774, 37th Joint Propulsion Conference,
Salt Lake City
. 6 H 05H 1/54, F 03H 1/00.
Gopanchuk V. V., Potapenko M. Yu.
Gas Breakdown, Hall or Stationary Plasma Thruster, Electrical Insulator.