US Patent 5,054,046 (Shoulders Plasma Deflection)
ID: shoulders-patent-5054046
Summary
Shoulders patent for plasma deflection and cleanup using EV technology. Granted October 1, 1991.
Overview
US Patent 5,054,046, granted on October 1, 1991, to inventor Kenneth R. Shoulders, outlines mechanisms for plasma deflection and surface cleanup utilizing high-density energy clump or 'Electrum Validum' (EV) technology. The patent details the generation, manipulation, and deflection of concentrated charge clusters through electromagnetic fields, establishing a technical framework for directing energetic plasmoids. This methodology intersects fundamentally with theoretical constructs such as the 50km Altitude Plasmoid and builds on historical plasma confinement milestones dating back to the 1958: Operation Hardtack I atmospheric tests. Within the patent's claims, Shoulders describes apparatus and methods to steer, neutralize, and disperse high-energy plasma formations, providing early foundational engineering for controlling localized charge envelopes. By articulating the physics necessary to deflect high-velocity charged particle bodies, the patent addressed long-standing instability problems first encountered in early accelerator research, including the concepts pioneered during the 1946: Astron Project Inception and the subsequent 1949: Christofilos conceives strong-focusing principle for accelerators. Consequently, US Patent 5,054,046 represents a vital documented bridge between empirical high-beta plasma dynamics and directed electromagnetic manipulation systems.
Significance
The technological architecture protected under US Patent 5,054,046 holds substantial significance for defense and advanced aerospace laboratories exploring high-energy plasma applications. The mechanisms described for deflecting and controlling coherent plasma clusters directly inform theoretical models concerning Aerodynamic Disruption and broader directed-energy defense concepts, such as the Anti-Satellite (ASAT) Plasma Weapon. Institutional research nodes like the Air Force Office of Scientific Research, Naval Air Systems Command, and NASA MSFC have historically tracked similar plasma containment and propulsion concepts to assess both defensive shielding and energetic payload dynamics. Furthermore, advanced aerospace contractors, including Lockheed Martin Skunk Works® and specialized plasma ventures like MSNW LLC, have explored the cross-applicability of compact plasmoid steering for space propulsion, material modification, and high-altitude aerodynamic disruption. By standardizing a method for the precise spatial deflection of high-charge-density formations, Patent 5,054,046 established an intellectual baseline for non-equilibrium plasma trajectory control across multiple military and aerospace research lineages.
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