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 the configuration of the core of the magnetization source of magnetic systems of electric propulsion
... distribution in an operating interpolar interval are presented.
1.
Гопанчук В. В.
Плазменный двигатель с замкнутым дрейфом электронов: пат. РФ №
2204053; кл. F03H 1/00; 29.09.00.
Gopanchuk V., Mitrofanova O., Potapenko M.
Hall effect thruster, stationary plasma thruster, hybrid plasma
thruster, magnetic system, magnetic coil.
155-162
Study of conditions of electric breakdown in the flow part of electrical insulators of electric propulsion propellant supply systems
...
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.
Gopanchuk V. V., Potapenko M. Yu.
Gas Breakdown, Hall or Stationary Plasma Thruster, Electrical Insulator.
131-137