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Hall-Effect Thruster Utilizing Bismuth as PropellantA laboratory-model Hall-effect spacecraft thruster was developed that utilizes bismuth as the propellant. Xenon was used in most prior Hall-effect thrusters. Bismuth is an attractive alternative because it has a larger atomic mass, a larger electron-impact-ionization cross-section, and is cheaper and more plentiful.
Document ID
20080047186
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Szabo, James
(Busek (J.) Co., Inc. MA, United States)
Gasdaska, Charles
(Busek (J.) Co., Inc. MA, United States)
Hruby, Vlad
(Busek (J.) Co., Inc. MA, United States)
Robin, Mike
(Busek (J.) Co., Inc. MA, United States)
Date Acquired
August 24, 2013
Publication Date
November 1, 2008
Publication Information
Publication: NASA Tech Briefs, November 2008
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
MFS-32440-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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