Review of Hall Thruster Plume Modeling
By Iain D. Boyd. 2001
139 citations recorded by the source corpus.
Subfields: Computer Networks and Communications, Electrical and Electronic Engineering
View Paper: https://www.semanticscholar.org/paper/2a7fb682f5f36923bfd7a7e8fb647c88a071d0b0
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In Computer Networks and Communications
In Electrical and Electronic Engineering
Citations in the corpus
- The Influence of Neutral Flow Rate in the Operation of Hall Thrusters. (2009, background): “Thruster..........................................................................................330 xxiii Nomenclature Constants e electron charge, 1.6022×10-19 [C] g gravitational acceleration, 9.8067 [m/s2] kB Boltzmann’s constant, 1.3807×10-23 [J/K] me mass of an electron, 9.1094×10-31 [kg] mxe”
- Development and characterization of high -efficiency, high -specific impulse xenon Hall thrusters. (2004, background): “Although significant progress has been made in recent years [138-140, 144, 147, 191-194], there presently are no analytic or numerical models of Hall thrusters that can accurately predict the performance parameters over a wide range of operating conditions.”