Discharge Characterization of the Coaxial Magnetoisolated Longitudinal Anode Hall Thruster-Reference-Cited by-同舟云学术

Discharge Characterization of the Coaxial Magnetoisolated Longitudinal Anode Hall Thruster

Published:2013-07 Issue:4 Volume:29 Page:938-949
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Kronhaus Igal¹,Kapulkin Alexander¹,Balabanov Vladimir¹,Rubanovich Maksim¹,Guelman Moshe¹,Natan Benveniste¹

Affiliation:

1. Electric Propulsion Laboratory, Asher Space Research Institute, Technion—Israel Institute of Technology, 32000 Haifa, Israel

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B34754

Reference21 articles.

1. AhedoE.GallardoJ. M. “Scaling Down Hall Thrusters,” IEPC Paper 2003-104, 2003.

2. Development of low power Hall thrusters

3. Low Power Cylindrical Hall Thruster Performance and Plume Properties

4. BelikovM. B.GorshkovO. A.DyshlyukE. N.LovtzovA. S.ShagaydaA. A. “Development of Low-Power Hall Thruster with Lifetime up to 3000 Hours,” IEPC Paper 2007-129, 2007.

5. LoyanA. V.MaksymenkoT. A. “Performance Investigation of SPT-20M Low Power Hall Effect Thruster,” IEPC Paper 2007-100, 2007.

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