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Inductive Plasma Accelerator—MSNW,
Dr. Timothy Ziemba,
Dr. John Slough, Business
Official, sloughj@comcast.net
DOE Grant No. DE-FG02-04ER84011
Amount: $652,500
For the plasma jet liner approach to magnetized target
fusion, a plasma accelerator is required that is capable of launching a plasma
jet with a mass of 0.2 mg to 0.4 mg and a diameter no larger than about 20
cm. In addition, the accelerator must be
capable of attaining plasma/plasmoid velocities in excess of 200 km/s, a timing
precision better than a microsecond down to nanoseconds, and a controllable
density profile of high uniformity and purity.
This project will achieve the
desired acceleration parameters by designing and constructing an inductive
plasmoid accelerator (IPA). In addition, two IPAs will be merged to form
a suitable target plasmoid that will be compressed to high density and
temperature with a suitable plasma liner, providing the first experimental test
of the plasma liner fusion concept. In
Phase I, the inductive plasma accelerator was analyzed analytically and
numerically to determine an optimal configuration for application to the plasma
liner approach to target fusion. A
complete design of the inductive plasma accelerator to be built was
executed. Additional analysis and design
was conducted on an experimental testbed for merging accelerated plasmoids and
compressing with a plasma liner. Phase
II will construct a plasmoid accelerator and produce a magnetized plasmoid that
is suitable for the formation of the target plasmoid as well as for later
compression by an array of similar plasmoids. An interaction chamber will be constucted that
is capable of producing a plasma liner for compression experiments. Simulations will be performed for all three
components of the experimental work: the
acceleration of two plasmoids, their merging, and the formation of a plasma
liner followed by the radial implosion of the plasma liner onto the colliding
plasmoids.
Commercial
Applications and Other Benefits as described by the awardee: The inductive
plasma accelerator (I