The development of a Sustained High Power Density (SHPD) facility

Journal Article · 08 March 2021 · Fusion Engineering and Design

DOI: https://doi.org/10.1016/j.fusengdes.2020.112214 · OSTI ID:1820349

Brown, T. ^[1]; Menard, J. E.  ^[1]; Zhai, Y.  ^[1]; Majeski, R. ^[1]; Rana, C. ^[1]; McIntyre, P.  ^[2]

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1. Princeton Plasma Physics Lab. (PPPL), Princeton, NJ (United States)
2. Texas A & M Univ., College Station, TX (United States); Accelerator Technology Corp., College Station, TX (United States)

A Sustained High Power Density (SHPD) facility is being planned within the U.S. as a non DT device which can be a bridge to a Compact Fusion Pilot Plant (CFPP) DT operated facility with the future capacity to produce a levelised cost of electricity at a rate competitive with current power generating systems. To accomplish this a review of ITER cost data and recent next step physics/engineering studies that promoted technology development, physics enhancements and innovated configuration improvements that increase operating availability have been injected into a proposed PPPL SHPD design. Much of the physics and engineering design basis for this effort centers on a series of ST studies carried out in recent years attempting to maximize the low aspect ratio (AR) ST performance within realistic engineering constraints of this compact fusion device. One issue found in the low AR design is the lack of volt-seconds generated by a small central solenoid that resides in the available space left after sizing the TF structure to support the high current density/HTS TF coil. Although not required in a larger pilot plant device, a solenoid wrapped around the plasma side of the SC TF coil was considered for the small low aspect ratio SHPD device. Adding a solenoid to the plasma side of the TF imposes a major change to the device configuration – a change which has been found to have cost and assembly issues when compared with an OH solenoid located at the machine center. Finally, the inclusion of a liquid metal first wall divertor system, the integration of local pairs of outboard DCLL blanket segments and a summary of physics performance conditions will be presented.

• Research Organization: Princeton Plasma Physics Laboratory (PPPL), Princeton, NJ (United States)
• Sponsoring Organization: USDOE
• Grant/Contract Number: AC02-09CH11466
• OSTI ID: 1820349
• Alternate ID(s): OSTI ID: 1815044
• Journal Information: Fusion Engineering and Design, Vol. 168; ISSN 0920-3796
• Publisher: ElsevierCopyright Statement
• Country of Publication: United States
• Language: English