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Comprehensive comparisons of the numerically simulated results of plasma flow fields in a 100-kW-class 2-D magnetoplasmadynamic thruster with the available experimental data are conducted. The propellant is argon of 1.25 g/s, and the discharge current is varied from 8 to 12 kA. The physical model includes a nonequilibrium single level of ionization and a collisional radiative model for argon ion to...
High-density energy conversion using a compact closed-cycle magnetohydrodynamics electrical power generator was described in this paper. Cesium-seeded argon gas was first used to demonstrate the conversion process. High power density (0.76 GW/m3 ) for outstanding efficient energy conversion was successful through the application of high- and uniform-density 4 T magnetic flux which enables high-Hall...
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