Cylindrical Hall Thrusters

Author:

Raitses Y.1,Smirnov Artem1,Fisch N.1

Affiliation:

1. Princeton Plasma Physics Laboratory1, Princeton University

Publisher

American Institute of Aeronautics and Astronautics

Reference31 articles.

1. A.I.MorozovandV.V.Savel'ev,inReviewsofPlasmaPhysics,editedbyB.B.KadomtsevandV.D.Shafranov, ( ConsultantsBureau,NewYork,2000),Vol.21,p.206.

2. V.Kim,J.Prop.Power14,736(1998).

3. V.KhaymsandM.Martinez-Sanches,inMicropropulsionforSmallSpacecraft,editedbyM.M.MicciandA.D. Ketsdever(AIAAProgress inAstronauticsandAeronautics, 2000),Vol.187,p.45.

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2. The effect of anode axial position on the performance of a miniaturized cylindrical Hall thruster with a cusp-type magnetic field;Plasma Science and Technology;2022-06-08

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4. Plasma detachment mechanisms in a magnetic nozzle;47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2011-07-31

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

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