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

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The elements of a thrust to develop liquid metal PFcs are also important <strong>for</strong> liquid metal flows in<br />

the blanket ducts contained in Thrust 13. They include:<br />

1. magnetohydrodynamic modeling of liquid metal transport at high hartmann and<br />

Reynolds numbers with fusion relevant fields, configuration and magnetic field gradients,<br />

including the effect of plasma mhd on the stability of liquid metals. This activity is a<br />

combination of theory, simulation and small laboratory experiments <strong>for</strong> validation.<br />

2. a multi-laboratory ef<strong>for</strong>t to investigate substrate optimization (<strong>for</strong> slowly flowing<br />

liquids), including capillary effects, as well as general chemical effects, temperature limits,<br />

corrosion (including corrosion of neutron-irradiated materials), wetting, etc., is needed.<br />

3. design and engineering of practical devices <strong>for</strong> injecting, controlling and removing liquid<br />

metals in the presence of fusion-relevant magnetic fields.<br />

4. design and engineering of systems to remove heat from liquid metal PFcs, <strong>for</strong> slowly<br />

flowing liquid metals. Fast flowing liquids (e.g., jets) would carry the heat load with the<br />

fluid.<br />

5. a comprehensive liquid metal test stand capability. an adequate test stand should include<br />

a liquid metal loop feeding and draining a target surface, with appropriate flow rates over<br />

the surface, at a relevant magnetic field, and field angle to the surface. high heat flux<br />

testing using e-beams or lasers should be available. The ability to per<strong>for</strong>m simultaneous<br />

Pmi studies, at least on a time scale appropriate to the residence time of the fluid on<br />

the target surface, is desirable. comprehensive diagnostics of the liquid metal surface<br />

behavior should be available.<br />

6. Following test stand qualification, a plasma confinement device should test these liquid<br />

metal systems with discharge durations in excess of the residence time of the fluid in the<br />

system.<br />

7. demonstration of high-power conversion efficiency using removed heat under demolike<br />

conditions.<br />

referenCes<br />

J.C. Mankins, “Technology Readiness Levels, A White Paper,” Advanced Concepts Office, Office of<br />

Space Access and Technology, NASA, April 6, 1995.<br />

D.L. Youchison and M.T. North, “Thermal Per<strong>for</strong>mance of a Dual-Channel, Helium-Cooled, Tungsten<br />

Heat Exchanger,” <strong>Fusion</strong> Technol. 39 2, 899-904 (2001).<br />

E. Diegele, R. Kruessmann, S. Malang, P. Norajitra, G. Rizzi, “Modular He-cooled divertor <strong>for</strong> power<br />

plant applications,” <strong>Fusion</strong> Eng. Des., 66-68, 383-387 (2003).<br />

R. Majeski et al., Phys. Rev. Lett. 97 07, 5002 (2006).<br />

A. Vertkov et al., <strong>Fusion</strong> Eng. Des., 82 15-24, 1627-1633 (2007).<br />

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