Fully Kinetic Modeling of Divergent Cusped Field Thrusters

Author:

Gildea Stephen,Batishchev Oleg,Martinez-Sanchez Manuel

Publisher

American Institute of Aeronautics and Astronautics

Reference19 articles.

1. 1Bober,A.S.,Kim,V.,etal.“StateofWorksonElectricalThrustersintheUSSR,”22ndInternational Electric Propulsion Conference, Viareggio, Italy, October 1991, also IEPC-91-003.

2. Spacecraft Electric Propulsion-An Overview

3. Main Physical Features and Processes Determining the Performance of Stationary Plasma Thrusters

4. 4Courtney, D.G.andMartínez-Sánchez, M. “DivergingCusped-FieldHallThruster(DCHT),”30thInternational Electric Propulsion Conference, FLorence, Italy, September 2007, also IEPC-2007-2039.

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1. Low Power Cusped Field Thruster Developed for the Space-Borne Gravitational Wave Detection Mission in China;Applied Sciences;2021-07-16

2. Full Particle-In-Cell Simulation Methodology for Axisymmetric Hall Effect Thrusters;Journal of Propulsion and Power;2014-01

3. Characterization and Optimization of a Diverging Cusped Field Thruster with a Calibrated Horizontal Accelerometer;47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2011-07-31

4. Ion Velocity Distribution in a Low-Power Cylindrical Hall Thruster;46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2010-07-25

5. Spectroscopic and Electrostatic Investigation of the Diverging Cusped-Field Thruster;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02

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