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Antares achieves zero-power criticality at INL
Leveraging more than $140 million in private capital fundraising, over 322,000 square feet of operational manufacturing space, and multifaceted partnerships with the Departments of Energy and Defense, reactor start-up Antares has become the first company involved in the Reactor Pilot Program to achieve zero-power fueled criticality—a full month ahead of the July 4 deadline set by President Trump’s Executive Order 14301.
This milestone, announced yesterday, was achieved with the company’s Mark-0: a sodium heat-pipe-cooled, TRISO-fueled microreactor. The Mark-0 is a forerunner to the company’s flagship design, which it calls the R1. For Antares, this development represents a key validation of its reactor physics, control systems, and supply chain.
Peter H. Titus, Charles Kessel
Fusion Science and Technology | Volume 77 | Number 7 | October-November 2021 | Pages 557-567
Technical Paper | doi.org/10.1080/15361055.2021.1898303
Articles are hosted by Taylor and Francis Online.
New superconductor types and performance levels are being developed and have enabled consideration of higher-field, smaller-size devices. In this paper, sizing options for the next Fusion Energy System Study (FESS) design study are explored. The 2016/2017 baseline Fusion Nuclear Science Facility (FNSF) used a bucked and wedged solution with a large external case mainly to support out-of-plane loads and allow radial servicing. Use of a larger case to provide inner leg compression may be needed for the higher-field, smaller devices. These structural concepts have been employed in FIRE, IGNITOR, and C-Mod. Each of these concepts will be investigated as candidates for a next machine study. Recommendations will be made as to how these concepts can be incorporated into systems codes.
The iterative design of the poloidal field coil system and the iterative choice of scenario currents are needed to go along with toroidal field (TF) coil support concepts. Concepts that employ a bucked solution require assessment of cancellation of the central solenoid radially outward and the TF radially inward load, and thus affect the sizing of both. Ideally better but simple structural models of the poloidal coils can be built into the scenario development codes to address advanced TF support schemes. Simplified spreadsheet assessments of structural concepts are presented, and these are benchmarked against finite element analyses. Possible options for the FNSF and next machine studies are assessed in terms of achievable fields and space allocation.