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Space Nuclear Power Systems - Direct Fusion Drive

机译:太空核动力系统-直接聚变驱动

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The Direct Fusion Drive (DFD) is a small fusion reactor that has the potential to revolutionize space power and propulsion. Direct Fusion Drive is based on the Princeton Field-Reversed Configuration reactor concept from Princeton Plasma Physics Laboratory. We have been using our NASA funding to explore the balance of plant for this unique engine, which can provide both megawatts of electric power and multi-Newtoris of thrust in a single integrated device. The engine has an array of field shaping coils with two smaller but higher field mirror coils. Coolant lines running along the fusion chambeer collect thermal energy from the neutrons, bremsstrahlung radiation, and synchrotron radiation for producing electricity. A kW neutral beam injects the fusion fuel into the center of the engine, while propellant enters from the ionizing gas box on the end opposite the nozzle. This paper will present the latest work on sizing a Brayton engine for DFD and compare a typical Xenon-Helium coolant engine to a supercritical carbon dioxide engine. The coolant lines for the thermal engine will need to run through the engine's shielding, which must absorb sufficient heat and neutrons to protect the superconductors and their cooling systems. This is a complex and interesting engineering problem, which we are addressing in parallel with development of the core fusion physics. The paper will begin with a short summary of the DFD technology. We will then present the latest work on sizing the Brayton engine, and comparing the Xenon-Helium option to supercritical carbon dioxide. We will then briefly review the preliminary design for the space radiators and provide a mass breakdown showing the estimated specific power achievable. Results on the RF generation system and on the power generators are also presented.
机译:直接聚变驱动器(DFD)是一种小型聚变反应堆,具有改变太空动力和推进力的潜力。直接聚变驱动器基于普林斯顿等离子体物理实验室的普林斯顿场反向配置反应堆概念。我们一直在利用美国宇航局的资金来探索这种独特发动机的设备平衡,该发动机可以在单个集成设备中提供兆瓦级的电力和多种新推力。该发动机具有一系列场成形线圈,其中有两个较小但较高的场镜线圈。沿着聚变斜角延伸的冷却液管线收集来自中子,致辐射和同步辐射的热能,以产生电能。一千瓦的中性束将聚变燃料注入发动机中心,而推进剂则从与喷嘴相对的一端的电离气体箱进入。本文将介绍为DFD确定布雷顿发动机尺寸的最新工作,并将典型的氙氦冷却剂发动机与超临界二氧化碳发动机进行比较。用于热力发动机的冷却剂管线将需要穿过发动机的护罩,该护罩必须吸收足够的热量和中子,以保护超导体及其冷却系统。这是一个复杂而有趣的工程问题,我们正在与核心聚变物理学的发展同时解决。本文将从DFD技术的简短摘要开始。然后,我们将介绍有关Brayton发动机的选型以及将Xenon-Helium选项与超临界二氧化碳进行比较的最新工作。然后,我们将简要回顾一下空间散热器的初步设计,并提供质量分解图,显示可达到的估计比功率。还介绍了RF生成系统和发电机的结果。

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