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Stabilization of high-compression, indirect-drive inertial confinement fusion implosions using a 4-shock adiabat-shaped drive

机译:使用4冲击绝热体形驱动器稳定高压缩,间接驱动的惯性约束聚变内爆

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摘要

Hydrodynamic instabilities and poor fuel compression are major factors for capsule performance degradation in ignition experiments on the National Ignition Facility. Using a recently developed laser drive profile with a decaying first shock to tune the ablative Richtmyer-Meshkov (ARM) instability and subsequent in-flight Rayleigh-Taylor growth, we have demonstrated reduced growth compared to the standard ignition pulse whilst maintaining conditions for a low fuel adiabat needed for increased compression. Using in-flight x-ray radiography of pre-machined modulations, the first growth measurements using this new ARM-tuned drive have demonstrated instability growth reduction of similar to 4x compared to the original design at a convergence ratio of similar to 2. Corresponding simulations give a fuel adiabat of similar to 1.6, similar to the original goal and consistent with ignition requirements. (C) 2015 AIP Publishing LLC.
机译:在国家点火装置上的点火实验中,流体动力学的不稳定性和不良的燃料压缩是导致胶囊性能下降的主要因素。使用最新开发的具有衰减的第一冲击的激光驱动曲线来调整烧蚀的Richtmyer-Meshkov(ARM)不稳定性以及随后的飞行中瑞利-泰勒生长,我们证明了与标准点火脉冲相比,生长减少了,同时保持了较低的条件增加压缩所需的燃料绝热材料。使用机加工调制的机载X射线射线照相技术,使用这种新的ARM调优驱动器进行的首次增长测量已证明,与原始设计相比,其收敛性降低了约2倍,不稳定增长减少了约4倍。相应的模拟给出一个类似于1.6的燃料绝热体,该绝热体与原始目标相似,并且符合点火要求。 (C)2015 AIP Publishing LLC。

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