Characterization of a One Hundred Watt, Long Lifetime Hall Effect Thruster for Small Spacecraft-Reference-Cited by-同舟云学术

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Characterization of a One Hundred Watt, Long Lifetime Hall Effect Thruster for Small Spacecraft

Published:2017-07-07 Issue: Volume: Page:
ISSN:
Container-title:53rd AIAA/SAE/ASEE Joint Propulsion Conference
language:
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Author:

Szabo James J.¹,Tedrake Rachel¹,Metivier Emily¹,Paintal Surjeet¹,Taillefer Zachary¹

Affiliation:

1. Busek Company, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4728

Reference35 articles.

1. Khayms, V. "Advanced Propulsion for Microsatellites," Ph.D. Dissertation,MIT Department of Aeronautics and Astronautics, 2000.

2. Warner, N. "Theoretical and Experimental Investigation of Hall Thruster Miniaturization," Ph.D. Dissertation,MIT Department of Aeronautics and Astronautics, 2007.

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3. Evaluation of a Planar Scandate Cathode for Hall Thruster Operation;AIAA SCITECH 2024 Forum;2024-01-04

4. Effects of Magnetic Field Configuration on the Performance of 100 W-Class Hall Thruster Using Carbon Dioxide;Lecture Notes in Networks and Systems;2024

5. Demonstration and experimental characteristics of a water-vapor Hall thruster;Journal of Electric Propulsion;2023-03-27

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