A Hall Thruster Performance Model Incorporating the Effects of a Multiply-Charged Plasma

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A Hall thruster performance model that predicts anode specific impulse, anode efficiency, and thrust is discussed. The model is derived as a function of a volta

A Hall Thruster Performance Model Incorporating the Effects of a Multiply-Charged Plasma

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Efficiency Analysis of a High-Specific Impulse Hall Thruster

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Performance and plasma measurements of the high-specific impulse NASA-173Mv2 Hall thruster were analyzed using a phenomenological performance model that account

Fundamentals of Electric Propulsion

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Throughout most of the twentieth century, electric propulsion was considered the technology of the future. Now, the future has arrived. This important new book

Laboratory Model 50 KW Hall Thruster

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