Characterizing the Exhaust Plume of the Three-Electrode Micro Pulsed Plasma Thrusters
Myeongkyo Seo
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Characterizing the Exhaust Plume of the Three-Electrode Micro Pulsed Plasma Thrusters

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Three-electrode micro-PPTs are a new version of two electrode micro-PPTs devices. Performance predictions and contamination expectations are essential characteristics needed by satellite designers. In order to focus on thruster specific impulse, thrust and efficiency, measuring the exhaust velocity or impulse bit and propellant consumption rate is essential. While this is not always possible to measure directly, focusing on the ejected mass from the PPT provides significant information allowing determination of these performance statistics. Specifically, focusing on exhaust angle distribution ...