用于惯性约束聚变靶壳的快速成形液体表面

R. Stephens
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引用次数: 1

摘要

先进的ICF目标将有固体或液体燃料的内层。它们的内表面必须光滑且无污染。目前生产这种表面的所有方法都存在一些问题:液体表面凹陷,固体表面容易出现小面,聚合物泡沫稳定表面被泡沫中的碳污染。另一种选择可能是在射击之前立即通过燃料饱和泡沫壁胶囊的快速热膨胀产生液体表面。这种方法利用了液氢相对于其泡沫基质的大膨胀系数。在冷却过程中,外壳被暴露在氢蒸气中填充;泡沫中的液体比自由液体的蒸汽压低,所以外壳会被完全填满。当外壳冷却时,它将保持在那个填充分数,并且它所含液体的密度增加。外壳可以冷冻并冷却到4k,以便可以在真空中储存和处理。当外壳受热时,液体膨胀;泡沫的弹性模量会迫使一些液体从表面流出。简单分析表明,在1 /spl mu/s内可形成1 /spl mu/m厚的液膜;这取决于泡沫的可压缩性及其细胞结构的流动阻力。表面张力会很快使这一表层平滑。在1000 /spl mu/s时,它不会开始下垂,因此有足够的时间使层达到令人满意的状态。分析将展示这种方法的可行性,以及它对壳壁结构和插射过程的约束。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Fast-formed liquid surfaces for inertial confinement fusion target shells
Advanced ICF targets will have an inner layer of solid or liquid fuel. Their inner surfaces must be smooth and contamination free. All of the current means to produce such a surface have problems: Liquid surfaces sag, solid surfaces tend to facet, and polymer-foam-stabilized surfaces are contaminated by carbon from the foam. An alternative may be to generate a liquid surface immediately before a shot by rapid thermal expansion of a fuel-saturated foam-walled capsule. This approach makes use of the large coefficient of expansion of liquid hydrogen relative to its foam matrix. The shell is filled by exposure to hydrogen vapor during cooling; liquid in the foam has a lower vapor pressure than free liquid, so the shell will fill to exactly 100%. It will stay at that fill fraction as the shell cools and the density of the liquid it contains increases. The shell may be frozen and cooled to 4 K so that it can be stored and handled in vacuum. When the shell is warmed, the liquid expands; the elastic modulus of the foam will force some liquid out of the surface. A simple analysis suggests that a 1 /spl mu/m thick liquid film might be generated in 1 /spl mu/s; that depends on the compressibility of the foam and the flow resistance of its cell structure. Surface tension would smooth this surface layer very rapidly. It would not begin to sag for 1000 /spl mu/s, so there would be sufficient time during which the layer would be satisfactory. An analysis will be presented showing the feasibility of this approach, and the constraints it puts on shell wall structure and insertion-and-shot procedures.
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