Development and Testing of a Prototype Bismuth Cathode for Hall Thrusters
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American Institute of Aeronautics and Astronautics
Reference2 articles.
1. 4Tverdokhlebov,O.S.,Semenkin,A.,andPolk,J."BismuthpropellantoptionforveryhighpowerTAL thruster,"AIAA-2002 -0348,40th AerospaceSciences Meeting, Reno, NV.
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