Ignition and Burn in a Hybrid Nuclear Fuel for a Pulsed Rocket Engine

被引:2
|
作者
Taylor, B. [1 ,2 ]
Cassibry, J. [2 ]
Adams, R. [1 ]
机构
[1] NASA, Marshall Space Flight Ctr, Huntsville, AL 35812 USA
[2] Univ Alabama, Prop Res Ctr, 301 Sparkman Dr, Huntsville, AL 35899 USA
关键词
Nuclear; Fission; Fusion; Advanced Propulsion; MAGNETIZED TARGET FUSION; PARAMETER SPACE;
D O I
10.1016/j.actaastro.2020.04.007
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This work explores the parameter space of a cylindrical hybrid nuclear fuel in support of a z-pinch driven pulsed fission-fusion (PuFF) engine. 0D power balance and 1D burn wave calculations have been performed to explore the parameter space of hybrid cylindrical nuclear fuels. The boundary of minimal initial conditions needed to reach breakeven are found within the context of the model. The effects of initial conditions upon the yield at the end of burn wave expansion are also determined. The model is used to examine the minimum initial energies predicted to result in yields of a few MJ. The goal of this work is to guide fuel design, inform future models and experiments as well as look for the most efficient parameter space for ignition in a z-pinch driven hybrid nuclear reaction. The impact of initial parameters upon ignition, burn, and gain are discussed. It is found that a hybrid cylindrical target may breakeven with initial energy near the axis of approximately 4-6 MJ in lithium deuteride/uranium 235 fuel. It is also found that magnetic field can lower the threshold further of which the magnitude changes across the parameter space. The dual fusion/fission reactions are found to boost each other leading to lower initial driving energies needed to reach breakeven in the hybrid cylindrical nuclear fuel.
引用
收藏
页码:465 / 475
页数:11
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