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Study on Compression of ICF Fuel in Rocket Model

机译:火箭模型中ICF燃料的压缩研究

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Compression of Inertial Confinement Fusion (ICF) fuel as required by Lawson Criterion has been of immense value in ICF studies. In this work, the order of compression has been studied on Rocket Model because a high-order reaction force responsible for compression may be seen to act as a rocket motion. It has been seen that the order of compression of lighter fuel such as D-T may be more effective if irradiated by high power Nd laser. The shocks produced as the reaction (Rocket effect) to the surface ablation generated by pulsed laser beams, compress the fuel which is estimated to be effective when the ratio of initial mass to the accelerated one is of the order of 5. The maximum achievable compression by a single strong shock is not more than 4 for a monatomic gas. For weak coalescing shocks to achieve adiabatic compression, the ablation efficiency is found to be maximum when target velocity equals nearly twice the ablation velocity. In such a case, the implosion efficiency of Rocket Model is found to be about 67 percent; neglecting heat loss.
机译:Lawson Criterion要求的惯性约束聚变(ICF)燃料压缩在ICF研究中具有巨大价值。在这项工作中,已经在火箭模型上研究了压缩的阶次,因为可以将负责压缩的高阶反作用力视为火箭的运动。已经看到,如果被大功率Nd激光器照射,则诸如D-T的较轻燃料的压缩顺序可能更有效。作为对脉冲激光束产生的表面烧蚀的反应(火箭效应)而产生的冲击会压缩燃料,这在初始质量与加速质量之比约为5时被认为是有效的。可实现的最大压缩对于单原子气体,单次强冲击的冲击力不超过4。对于弱聚结冲击以达到绝热压缩,当目标速度几乎等于消融速度的两倍时,消融效率最高。在这种情况下,火箭模型的内爆效率约为67%。忽略热量损失。

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