Performance and High-Speed Characterization of a 100-kW Nested Hall Thruster
- 1 January 2022
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 38 (1), 40-50
- https://doi.org/10.2514/1.b38080
Abstract
The performance of a three-channel, 100-kW nested Hall thruster was evaluated on xenon propellant for total powers up to 102 kW. The thruster demonstrated stable operation in all seven available channel combinations at discharge voltages from 300 to 500 V and three different current densities. The resulting test matrix contained forty-six unique conditions ranging from 5 to 102 kW total power and 16 to 247 A discharge current. At each operating condition, thrust, specific impulse, and efficiency were characterized. All seven channel combinations showed similar performance at a given discharge voltage and current density. The largest thrust recorded was at discharge voltage. Total efficiency and specific impulse ranged from 0.54 to and from 1800 to 2650 s s, respectively. Discharge current oscillations were also characterized with peak-to-peak values and with high-speed camera analysis, which provide insight into how the discharge channels oscillate and how those oscillations are affected by the presence of other operating channels. These results are discussed in the context of differences between single- and multichannel operation, as are the implications for the general viability of nested Hall thruster technology for future mission applications.
Keywords
Funding Information
- National Aeronautics and Space Administration (NNH16CP17C, NNX14AL67H, NNX15AQ43H, NNX16AM96H)
This publication has 19 references indexed in Scilit:
- Reduction of Energetic Ion Production in Hollow Cathodes by External Gas InjectionJournal of Propulsion and Power, 2013
- Mass and Cost Model for Selecting Thruster Size in Electric Propulsion SystemsJournal of Propulsion and Power, 2013
- Hall Thruster Cathode Flow Impact on Coupling Voltage and Cathode LifeJournal of Propulsion and Power, 2012
- Cross-field electron transport induced by a rotating spoke in a cylindrical Hall thrusterPhysics of Plasmas, 2012
- Hall-Effect Thruster--Cathode Coupling, Part I: Efficiency Improvements from an Extended Outer PoleJournal of Propulsion and Power, 2011
- High-power, null-type, inverted pendulum thrust standReview of Scientific Instruments, 2009
- Potential fluctuations and energetic ion production in hollow cathode dischargesPhysics of Plasmas, 2007
- Effects of Cathode Configuration on Hall Thruster Cluster Plume PropertiesJournal of Propulsion and Power, 2007
- Plasma oscillations in Hall thrustersPhysics of Plasmas, 2001
- Thrust stand for high-power electric propulsion devicesReview of Scientific Instruments, 1991