Performance characteristics of a 5 kW laboratory Hall thruster-Reference-Cited by-同舟云学术

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Performance characteristics of a 5 kW laboratory Hall thruster

Published:1998-07-13 Issue: Volume: Page:
ISSN:
Container-title:34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Haas James¹,Gulczinski, III Frank¹,Gallimore Alec¹,Spanjers Gregory²,Spores Ronald²

Affiliation:

1. Michigan, Univ., Ann Arbor

2. USAF, Electric Propulsion Lab., Edwards AFB, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3503

Reference15 articles.

1. Analysis of Hall-effect thrusters and ion engines for orbit transfer missions

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1. Effects of Magnetic Field Gradient on the Performance of a Magnetically Shielded Hall Thruster;Aerospace;2023-11-05

2. Electrical Facility Effects on Hall Thruster Cathode Coupling: Performance and Plume Properties;Journal of Propulsion and Power;2016-01

3. Validating a Plasma Momentum Flux Sensor to an Inverted Pendulum Thrust Stand;Journal of Propulsion and Power;2009-05

4. Hall Thruster and VASIMR VX-100 Force measurements using a Plasma Momentum Flux Sensor;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

5. Far-Field Species Distribution Measurements on the BHT-600 Hall Thruster Cluster;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08

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