Solutions for discharge chamber sputtering and anode deposit spalling in small mercury ion thrusters
Small electron bombardment mercury ion thrusters are considered for attitude-control and station-keeping operations in the case of earth synchronous satellites. The required operational lifetimes of the order of 20,000 hours could present problems because of the occurrence of sputter erosion of thruster discharge chamber components. The investigation reported is concerned with a study of these problems and the development of approaches for overcoming them.