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タイトルMagnetized Target Fusion Driven by Plasma Liners
本文(外部サイト)http://hdl.handle.net/2060/20010067645
著者(英)Smith, James; Schmidt, George; Knapp, Charles E.; Turchi, Peter J.; Kirkpatrick, Ronald C.; Lee, Michael; Richeson, Jeff; Thio, Y. C. Francis; Rodgers, Stephen L.; Eskridge, Richard
著者所属(英)NASA Marshall Space Flight Center
発行日2001-01-01
言語eng
内容記述Magnetized target fusion (MTF) attempts to combine the favorable attributes of magnetic confinement fusion (MCF) for energy confinement with the attributes of inertial confinement fusion (ICF) for efficient compression heating and wall-free containment of the fusing plasma. It uses a material liner to compress and contain a magnetized plasma. For practical applications, standoff drivers to deliver the imploding momentum flux to the target plasma remotely are required. Spherically converging plasma jets have been proposed as standoff drivers for this purpose. The concept involves the dynamic formation of a spherical plasma liner by the merging of plasma jets, and the use of the liner so formed to compress a spheromak or a field reversed configuration (FRC). For the successful implementation of the scheme, plasma jets of the requisite momentum flux density need to be produced. Their transport over sufficiently large distances (a few meters) needs to be assured. When they collide and merge into a liner, relative differences in velocity, density and temperature of the jets could give rise to instabilities in the development of the liner. Variation in the jet properties must be controlled to ensure that the growth rate of the instabilities are not significant over the time scale of the liner formation before engaging with the target plasma. On impact with the target plasma, some plasma interpenetration might occur between the liner and the target. The operating parameter space needs to be identified to ensure that a reasonably robust and conducting contact surface is formed between the liner and the target. A mismatch in the "impedance" between the liner and the target plasma could give rise to undesirable shock heating of the liner leading to increased entropy (thermal losses) in the liner. Any irregularities in the liner will accentuate the Rayleigh-Taylor instabilities during the compression of the target plasma by the liner.
NASA分類Plasma Physics
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/226101


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