Investigation of discharge chamber insulator relative erosion of stationary plasma thruster
The results of investigations of relative erosion at different modes of the stationary plasma thruster operation are presented herein. The optimal parameters of thruster operation mode ensuring minimum erosion of the discharge chamber walls are defined herein.
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To the question of creating a stationary plasma engine of increased power
... a 20 kW Hall Effect Thruster // IEPC-2011-020
15. Leporini A., Giannetti V., Andreussi T. et al. Development of a 20 kW-class hall effect thruster // Space Pripulsion. Rome, 2016.
Pyatykh I., Rumyantsev A.
stationary plasma thruster, spacecraft, discharge chamber, vacuum stand
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