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Point-Source Helicity Injection Startup

Point-Source Helicity Injection Startup. Capabilities are being explored for NSTX-U… ~1 MA startup plasma, appropriate for OH, NBI, and/or RF sustainment Well-defined startup procedures and plasma development scenarios Unobtrusive and retractable injection hardware

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Point-Source Helicity Injection Startup

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  1. Point-Source Helicity Injection Startup • Capabilities are being explored for NSTX-U… • ~1 MA startup plasma, appropriate for OH, NBI, and/or RF sustainment • Well-defined startup procedures and plasma development scenarios • Unobtrusive and retractable injection hardware • Pegasus results are evolving the conceptual design: • Arc gun needed to generate the “seed” plasma • Formation of the poloidal field null is sensitive the geometry • Outer-PF induction provides finite Volt-seconds • Passive electrodes may be the optimum tool for providing maximum effective Volt-seconds with high Taylor limit for Ip • Electrodes and guns require different fuelling → active gas control • Local limiters mitigate impurities (Pegasus Zeff≤ 2 during HI; ~1 in OH) A. J. Redd, NSTX-U Facility Brainstorming Meeting, Feb 8, 2012

  2. Conceptual design for the NSTX-U startup system • Gun/electrode injector: • Single 8+ inch port off midplane • Retractable behind gate valve • Combines gun with large electrode • Piezoelectric gas control • Local limiter structure • Power supplies: • Bias comparable to Pegasus (1-2 kV; 15 kA; Dt ~ 1 ms) • Arc plasma uses simple PFN supply • Robust operating scenarios • Especially null formation and Ip buildup • Pegasus experiments informing and validating scenario development A. J. Redd, NSTX-U Facility Brainstorming Meeting, Feb 8, 2012

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