Study of the configuration of the hybrid plasma thruster discharge chamber
Aerospace propulsion engineering
Experimental Design Bureau “Fakel”, 181, Moskovsky av, Kaliningrad, 236001, Russia
AbstractResults of researches on the impact of the discharge chamber configuration hybrid plasma thruster on operation and characteristics to increase stability of specific parameters and characteristics in the models of different dimension types within the range of operating power of 100 w to 2.3 kw, including operating modes at high discharge voltage are presented.
Keywords:hall effect thruster; hybrid plasma thruster; discharge chamber; current oscillations.