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On the efficacy of imploding plasma liners for magnetized fusion target compression

机译:关于内爆等离子体衬套对磁化聚变靶压缩的功效

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A new theoretical model is formulated to study the idea of merging a spherical array of converging plasma jets to form a "plasma liner" that further converges to compress a magnetized plasma target to fusion conditions [Y. C. F. Thio , "Magnetized target fusion in a spheroidal geometry with standoff drivers," Current Trends in International Fusion Research II, edited by E. Panarella (National Research Council Canada, Ottawa, Canada, 1999)]. For a spherically imploding plasma liner shell with high initial Mach number (M=liner speed/sound speed) the rise in liner density with decreasing radius r goes as rho similar to 1/r(2), for any constant adiabatic index gamma=d ln p/d ln rho. Accordingly, spherical convergence amplifies the ram pressure of the liner on target by the factor A similar to C-2, indicating strong coupling to its radial convergence C=r(m)/R, where r(m)(R)=jet merging radius (compressed target radius), and A=compressed target pressure/initial liner ram pressure. Deuterium-tritium (DT) plasma liners with initial velocity similar to 100 km/s and gamma=5/3, need to be hypersonic M similar to 60 and thus cold in order to realize values of A similar to 10(4) necessary for target ignition. For optically thick DT liners, T < 2 eV, n>10(19)-10(20) cm(-3), blackbody radiative cooling is appreciable and may counteract compressional heating during the later stages of the implosion. The fluid then behaves as if the adiabatic index were depressed below 5/3, which in turn means that the same amplification A=1.6x10(4) can be accomplished with a reduced initial Mach number M approximate to 12.7(gamma-0.3)(4.86), valid in the range (10 < M < 60). Analytical calculations indicate that the hydrodynamic efficiency for plasma liners assembled by current and anticipated plasma jets is < 4%. A new similarity model for fusion alpha-particle heating of the collapsed liner indicates that "spark" ignition of the DT liner fuel does not appear to be possible for magnetized fusion targets with typical threshold values of areal density rho R < 0.02 g cm(-2). (c) 2008 American Institute of Physics.
机译:建立了一个新的理论模型来研究融合​​会聚等离子体射流的球形阵列以形成“等离子体衬里”的想法,该等离子体衬里进一步会聚以将磁化等离子体靶压缩到聚变条件[Y。 C. F. Thio,“带有对撞驱动器的球形几何体中的磁化目标融合”,国际融合研究II的当前趋势,由E. Panarella编辑(加拿大国家研究委员会,加拿大渥太华,1999年)。对于具有高初始马赫数(M =线性速度/声速)的球形内爆等离子体衬里壳,对于任何恒定的绝热系数gamma = d,随着半径r减小,衬里密度的增加与r / r(2)相似。 ln p / d ln rho。因此,球面会聚将衬套对目标的冲压压力放大了类似于C-2的系数A,表明与其径向会聚紧密耦合C = r(m)/ R,其中r(m)(R)=喷射合并半径(压缩的目标半径),A =压缩的目标压力/初始衬套压力。初始速度类似于100 km / s且gamma = 5/3的氘plasma(DT)等离子体衬管必须是类似于60的高超音速M,因此必须冷,以实现类似于10(4)所需的A值目标点火。对于光学厚度较厚的DT衬里,T <2 eV,n> 10(19)-10(20)cm(-3),黑体辐射冷却是可观的,并且可以抵消内爆后期的压缩加热。流体的行为就好像绝热指数被压低到5/3以下,这反过来意味着相同的放大倍数A = 1.6x10(4)可以通过将初始马赫数M降低至大约12.7(γ-0.3)( 4.86),有效范围为(10

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