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Research Needs for Magnetic Fusion Energy Sciences - US Burning ...

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estal into the core. We must also demonstrate that the required control launchers can be designed<br />

and operated to accommodate a high heat flux environment with high first-wall temperatures.<br />

another aspect of control developed in Thrust 2 that must be shown to be compatible with the<br />

demo heat flux environment is the control, avoidance, and mitigation of heat flux transients<br />

such as those from edge localized modes (elms) and disruptions. The energy released in an uncontrolled<br />

demo elm is likely to be ~ 4 x that of iteR where control techniques are already required<br />

to reduce the energy released in an elm by ~ 90%. disruptions as well must be essentially<br />

eliminated in a demo. techniques <strong>for</strong> avoiding, or suppressing, these transients must be deployed<br />

in a manner consistent with both a robust edge pedestal and control of the steady heat flux<br />

to PFcs.<br />

The high temperatures of PFcs that are envisioned in aRies designs (500-1000 o c) to make the<br />

fusion power cycle more thermally efficient also bring new challenges and opportunities. The<br />

challenge is that the PFc materials and technologies to be used at such high temperatures are<br />

both at their heat load handling limits and have a narrow temperature operational window. The<br />

opportunity associated with high-temperature PFcs is to study hydrogenic retention and control<br />

the tritium fuel cycle; in a demo reactor less than 1 in 100,000 t ions striking the wall can be retained<br />

in the material. That should be contrasted with current devices where this ratio is found to<br />

typically be only ~1 in 100. The high hydrogenic diffusion and reaction rates at demo PFc temperatures<br />

will greatly aid removal of fuel ions from PFc surfaces and allow demonstration of the<br />

fuel control required <strong>for</strong> demo. The intense steady and transient loads on the PFcs, however, will<br />

result in dust production. dust needs to be well-controlled <strong>for</strong> safety reasons in demo.<br />

The flux of fusion neutrons also represents a great challenge <strong>for</strong> a demo reactor’s PFc materials.<br />

While the neutron damage in the bulk PFc material may lead to increased tritium retention, the<br />

main impact of neutron irradiation is on thermal conductivity and brittleness, which affect the<br />

necessary thickness and structural integrity of the PFc components. For this reason the effects of<br />

neutrons are largely separable from the plasma-wall processes and resulting interaction with core<br />

plasma operation. ef<strong>for</strong>ts to address the effect of neutrons on PFcs are encompassed in Thrusts<br />

11 and 13.<br />

initial analysis of the Machine Characteristics Required <strong>for</strong> this Thrust<br />

The first task <strong>for</strong> designing a facility to support the central goal of this Thrust, demonstration of<br />

an integrated solution <strong>for</strong> the core and boundary, is to develop the requirements <strong>for</strong> such a facility’s<br />

optimal scientific and technical capabilities. The first of these characteristics is the power<br />

density. There are two metrics that the community often uses <strong>for</strong> comparing the power density<br />

across devices (table 1). Their different scalings reflect different heat flux issues and the large uncertainty<br />

in our present understanding. The first of these, P/s, is the average power through the<br />

surface of the plasma at its edge. The second metric, P/R, which assumes a constant width of heat<br />

flux in the boundary plasma, represents a more conservative projection to iteR and demo. a facility<br />

to support this Thrust should be designed <strong>for</strong> power flows into the edge and to the PFcs approaching<br />

demo levels (table 1). Further work on heat flux width scaling, such as that now ongoing,<br />

and that proposed in Thrust 9, will lead to improved estimates of expected heat flux profiles<br />

that can be taken into account <strong>for</strong> specification of the heating power requirement.<br />

327

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