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Crazy Fox wrote: Further details on previous posting.
The working (cavitating fluid) is a negatively charged salt water ( B(OH)3 + NaCl ) in non conducting oil emulsion. This constitutes a Zwitterionic micelles in non conducting negatively charged oil. When sprayed in a stream from the Heron reaction nozzles (previous post) the cavitation implosion creates a triple pulsed sequence. The second pulse is super hot and meets the IEC ideal fusion temperature for Boron 11 and Hydrogen. This is done on a molecular scale and avoids the issues Dr. Bussard encountered during his research.
The Poisson-Boltzmann equation allows for the partition of the surface potential between electolytes. The selectivity parameter have been determined by assuming agreement between the zeta potential determined by capillary electrophoresis and the calculated outer surface potential of the micelles.
The hydraulic apparatus of helical drag pump with open channels to case and Heron reaction nozzles combined with a return flow (Back Stroke) Francis turbine through a hollow drive shaft produces very high output shaft torque at low rpm. The low cost of manufacture of this type of engine is obvious and with the added fusion process and efficiency is unique.
How is the Coulomb Barrier (Kinetic Limit) to fusion overcome in this method? The Inertial Electrostatic charge Shell Vortex on an elongated nanomicelles implosion become r-f coupled with spin-spin coupled boron and hydrogen ions to induce a helical electron spin allowing a boron proton to fuse with hydrogen nuclei. W. Guglinski authored a book on Quantum Ring Theory that addresses this issue of Kinetic Limit. CANR (Chemical Assisted Nucleat Reaction) in the above method is dependent upon the coupling of the confinement shell and the internal plasma of borohydrogen . In German “Zwitterbewegung” resonant coupling of the borohydrogen plasma with it’s Inertial Confinement Shell is responsible for fusion at temperatures well below what is predicted by accepted theory.
A Colloid Mill Drag Pump with a reaction flow driving it and a backstroke return flow turbine adding additional torque make this method and apparatus a viable engine concept.
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