Characterization of a Pulsed Plasma Thruster Plume Using a Quadruple Langmuir Probe Method
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American Institute of Aeronautics and Astronautics
Reference29 articles.
1. Pulsed plasma microthruster propulsion system for synchronous orbit satellite
2. Analysis of solid Teflon pulsed plasma thruster
3. Exhaust Velocity Studies of a Solid Teflon Pulsed Plasma Thruster
4. Interferometric Density Measurements in the Arc of a Pulsed Plasma Thruster
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1. Discharge and Impulse Bit Characteristics of Pulsed Plasma Thruster with PTFE-Based Modified Propellants;Springer Proceedings in Physics;2023
2. Mathematical Modeling of a High Efficiency Pulsed Plasma Thruster for Microsatellites;57th International Astronautical Congress;2006-10-02
3. Preliminary Design and Analysis of a Directional Micro-Retarding Potential Analyzer for High-density Plumes;39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26
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