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Xenon-135m in Nuclear Thermal Propulsion

机译:Xenon-135m用于核热推进

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There has been recent interest at NASA for developing Nuclear Thermal Propulsion (NTP) to support a human Mars mission in the 2030's time frame. NTP offers superior performance over chemical propulsion systems and can greatly reduce the overall mass (and therefore cost) and travel time of a Human Mars mission. This work investigates the effect of the metastable state of ~(135)Xe (~(135m)Xe) on the operation of thermal NTP systems. Current models indicate that ~(135m)Xe has an appreciably larger absorption cross-section than the ground state of ~(135)Xe but ~(135m)Xe only has a 15.3 minute half-life. NTP systems work in a unique high power density, medium time length regime where the effect of ~(135m)Xe has a notable effect on the reactivity of the NTP reactor. In LEU graphite composite SULEU NTP systems it was found that the maximum decrease in reactivity during operation was 62.8 % greater when ~(135m)Xe was included in the burn up model. In LEU tungsten cermet SCCTE NTP systems, it was found that the maximum decrease in reactivity during operation was 93.1% greater when ~(135m)Xe was included in the burn up model. This work was accomplished with infinite lattice calculations in Serpent 2 and the TENDL 2014 nuclear library cross-sections for ~(135m)Xe. Understanding the effects of ~(135m)Xe and generating validated cross sections for ~(135m)Xe will be important in developing NTP control systems.
机译:美国宇航局最近对开发核热推进(NTP)以支持人类在2030年的火星任务感兴趣。 NTP具有优于化学推进系统的性能,并且可以大大减少人类火星飞行任务的总体质量(从而降低成本)和旅行时间。这项工作研究了〜(135)Xe(〜(135m)Xe)的亚稳态对热NTP系统运行的影响。当前模型表明,〜(135m)Xe的吸收截面比〜(135)Xe的基态大得多,但〜(135m)Xe的半衰期仅为15.3分钟。 NTP系统以独特的高功率密度,中等时间长度的方式工作,其中〜(135m)Xe的影响对NTP反应器的反应性具有显着影响。在LEU石墨复合材料SULEU NTP系统中,当在燃耗模型中包含〜(135m)Xe时,操作过程中反应性的最大降低幅度最大为62.8%。在LEU钨金属陶瓷SCCTE NTP系统中,发现在燃耗模型中包含〜(135m)Xe时,操作过程中反应性的最大降低幅度最大为93.1%。这项工作是通过在Serpent 2和〜(135m)Xe的TENDL 2014核库横截面中进行无限晶格计算来完成的。了解〜(135m)Xe的效果并生成〜(135m)Xe的有效横截面对于开发NTP控制系统非常重要。

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