Operation of Hall thrusters with bismuth propellant has been shown to be a promising path for development of high-power (140 kW per thruster), high performance (8000s I(sub sp at >70% efficiency) electric propulsion systems.
Flow Control of Liquid Metal Propellants for In-Space Electric Propulsion Systems
40th Fluid Dynamics Conference and Exhibit ; 2010 ; Chicago, IL, United States
28.06.2010
Aufsatz (Konferenz)
Keine Angabe
Englisch
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