Hall Current Plasma Source Having a Center-Mounted or a Surface-Mounted Cathode

• Published in: NASA Center for AeroSpace Information (CASI). Misc. Resources
• Main Authors: Martinez, Rafael A, Williams, John D, Moritz, Jr, Joel A, Farnell, Casey C
• Format: Web Resource
• Language: English
• Published: Hampton NASA/Langley Research Center 03.04.2018
• Subjects: Hollow cathodes; Magnetic shielding; Plasma; Plasma processing; Power supplies; Propulsion systems; Spacecraft; Spacecraft shielding; Thin films

A miniature Hall current plasma source apparatus having magnetic shielding of the walls from ionized plasma, an integrated discharge channel and gas distributor, an instant-start hollow cathode mounted to the plasma source, and an externally mounted keeper, is described. The apparatus offers advantages over other Hall current plasma sources having similar power levels, including: lower mass, longer lifetime, lower part count including fewer power supplies, and the ability to be continuously adjustable to lower average power levels using pulsed operation and adjustment of the pulse duty cycle. The Hall current plasma source can provide propulsion for small spacecraft that either do not have sufficient power to accommodate a propulsion system or do not have available volume to incorporate the larger propulsion systems currently available. The present low-power Hall current plasma source can be used to provide energetic ions to assist the deposition of thin films in plasma processing applications.