American Nuclear Society

Home / Publications / Journals / Fusion Science and Technology / Volume 35 / Number 3

High-Velocity Liquid Jet Injection into Tokamak Plasmas for Disruption Mitigation

Paul B. Parks, Marshall N. Rosenbluth, Sergei V. Putvinski, Todd E. Evans

Fusion Science and Technology / Volume 35 / Number 3 / May 1999 / Pages 267-279

Technical Paper

Proposed is a new concept for disruption mitigation and fast shutdown in tokamaks: the injection of hydrogen or helium liquid jets. Liquid jets can rapidly cool the plasma to reduce divertor heat loads and large halo current forces while simultaneously raising the density sufficiently to prevent runaway electron generation. Massive ~40- to 100-fold density increases equivalent to ~50 g of deuterium are necessary for this purpose in the International Thermonuclear Experimental Reactor (ITER). It is shown that only two or three simultaneously injected high-velocity (800 to 1200 m/s) jets can easily deliver this amount of fuel within a period of ~20 ms and thus avoid runaway electron buildup during the 50- to 500-ms current quench phase. Optimum jet parameters, such as radius, velocity, driving pressure, and injection time, predicted from a jet ablation/penetration model, lead to an innovative pulsed injector design concept. The design concept is also based on a thermodynamic process path that allows the lowest possible temperature at the nozzle orifice, given the constraint of a high, ~700-atm driving pressure. By having a cold jet exit the nozzle orifice, the potential problem of rapid boiling (flashover) during jet propagation across vacuum space between the nozzle orifice and the tokamak plasma can be overcome. A one-dimensional fluid-dynamic calculation, including finite compressibility, shows that a specially designed liquid Laval nozzle is needed for liquid helium injection because the jet velocity is supersonic (Mach number ~4). This injector concept is being considered for a proposed disruption mitigation experiment on DIII-D.

Questions or comments about the site? Contact the ANS Webmaster.