Hall effect thrusters for small-sized spacecrafts
- Pages
- 60-67
Abstract
The results of investigation tests and comparative analysis of various low-power Electric Propulsion (EP) designed for their 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.
Reference
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 М. Ю. Оптимизация магнитных систем электрореактивных двигателей // Вестник Московского авиационного института. 2011. Т. 18, № 1. С. 64—74.