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

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The plasma facing components in a demo reactor will face much more extreme boundary plasma<br />

conditions and operating requirements than any present or planned experiment, including iteR<br />

and the superconducting tokamaks abroad. The gap between current and planned tokamaks and<br />

demo in the area of compatible core-edge solutions is very large in terms of steady-state handling<br />

of demo-level power efflux on high-temperature material surfaces. This gap needs to be<br />

bridged in a manner consistent with external control of plasma current, heating, and fueling to<br />

maintain an optimized clean, hot and dense core plasma. The configurational flexibility and complete<br />

diagnostic coverage that will be needed <strong>for</strong> testing solutions <strong>for</strong> this demanding environment<br />

would be most readily accomplished in a limited activation facility. The knowledge gained<br />

from this research program would accelerate the development of integrated core-boundary solutions<br />

<strong>for</strong> high-fluence burning plasmas such as in a <strong>Fusion</strong> nuclear science Facility (FnsF), and a<br />

demonstration (demo) fusion power plant.<br />

solutions <strong>for</strong> individual challenges outlined should be addressed by several thrusts to in<strong>for</strong>m the<br />

design of the facility to support Thrust 12. The physics of the boundary layer plasma and methods<br />

to disperse the heat flux over a greater surface area are to be investigated in Thrust 9. Physics of<br />

the plasma surface interaction are to be investigated in Thrust 10. heat removal technologies and<br />

components will be developed in Thrust 11. The effects of neutrons will be tested in Thrusts 11<br />

and 13. techniques <strong>for</strong> limiting heat flux transients will be developed in Thrust 2, and methods<br />

<strong>for</strong> core plasma sustainment and control will developed in Thrust 5. however, there is no present<br />

or planned facility where these solutions can be combined and the complex interaction of these issues<br />

studied and tested at demo-like conditions: this is the central goal of Thrust 12.<br />

Primary Challenges <strong>for</strong> a DEMO boundary Configuration<br />

The most basic of physical conditions that a demo fusion power plant must accommodate is<br />

the very high heat efflux from the burning plasma core that arrives on PFc surfaces. For typical<br />

demo designs, the total power flowing that must be exhausted onto material surfaces is approximately<br />

four times that predicted <strong>for</strong> iteR, yet in a device of similar physical dimensions. since<br />

iteR’s PFcs are already at the limits of engineering design, new techniques <strong>for</strong> spreading the exhaust<br />

heat flux over as much of the vessel surface as possible must be developed <strong>for</strong> demo.<br />

simultaneous with such high-power handling requirements, demo will have a much higher<br />

duty factor (≥80%) than existing or planned devices, resulting in an annual energy and particle<br />

throughput 100-200 times greater than <strong>for</strong> iteR. such constant high loading would lead to macroscopic<br />

levels of erosion of PFc material, which will be thin (~ 5 mm) <strong>for</strong> reasons of heat removal<br />

and tritium breeding. an associated concern is that the eroded material may redeposit with poor<br />

thermal and mechanical properties.<br />

While various aspects of demo heat flux solutions will be developed in Thrusts 9, 10 and 11, the<br />

PFc surface designs and operational techniques must be shown to be compatible with a robust edge<br />

pedestal that assures high core confinement and simultaneously allows efficient core control techniques.<br />

steady-state operation will require external means of driving plasma current, fueling the<br />

core plasma and, ideally, optimizing the core plasma profiles. an important core-edge issue is the<br />

efficient coupling of the control carrier (e.g., waves) through a “thick” edge and collisionless ped-<br />

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