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This record contains the theoretical framework for the Aetherion Plasm room-temperature superconducting quantumelectrohydrodynamic (RTS-QEHD) metasystem for electrodeless atmospheric propulsion. The framework presents a formally consistent set of governing equations,closure relations, boundary conditions, and scaling constraints for anair-breathing, electrodeless propulsion concept combining superconductingmagnetic energy storage (SMES), pulse power, high-temperature orroom-temperature superconducting coils, metamaterial magnetic fluxconcentrators, macroscopic graphene architectures, andquantum-electrohydrodynamic (QEHD) plasma acceleration. The proposed architecture separates air intake and pre-ionization fromelectromagnetic acceleration. This separation is intended to reduce electrodeerosion, suppress stochastic breakdown, and provide a more deterministicplasma-generation pathway before electromagnetic momentum addition. Contents:- Maxwell-Lorentz electrodynamics and Maxwell stress formulation- Control-volume thrust balance- Fluid, drift-diffusion, MHD, and QEHD governing equations- Townsend avalanche, Paschen breakdown, attachment, recombination, and ionization closures- RF power deposition and electron-energy closure- Ginzburg-Landau and London superconductivity constraints- Metamaterial magnetic flux concentration via anisotropic permeability tensors- Fowler-Nordheim field emission and ADK-type tunneling-ionization scaling- Fourier stability, FDTD/PIC numerical discretization, and dimensionless plasma parameters- Illustrative one-dimensional pre-ionization case study- Sensitivity analysis with respect to the effective electron loss frequency- Representative electromagnetic body-force estimate for a 10 T superconducting field and a 1 kV/m acceleration field- Explicit caveats concerning Hall current, back-EMF, propulsive efficiency, magnetic pressure, and superconducting critical limits Scope and limitations:The record is intended as a simulation scaffold and feasibility-inequalityframework. It does not claim experimental validation, device completion, orthe existence of a commercially available room-temperature superconductor.Room-temperature superconductivity is treated as a target material class; thesame mathematical structure reduces directly to high-temperaturesuperconducting implementations such as REBCO, Bi-2212, or MgB2 systems. Keyword : electrodeless atmospheric plasma propulsion, RTS-QEHD metasystem, Aetherion Plasm, room-temperature superconducting propulsion framework, high-temperature superconducting plasma accelerator, metamaterial magnetic flux concentrator, anisotropic permeability tensor for magnetic concentration, macroscopic graphene plasma electrode, graphene field-emission architecture, RF pre-ionization for atmospheric propulsion, DBD pre-ionization plasma seeding, electromagnetic body force in weakly ionized air, Lorentz force density estimate for plasma propulsion, Hall current in magnetized atmospheric plasma, back-EMF in MHD accelerator, magnetic pressure constraint in superconducting propulsion, quantum electrohydrodynamic correction in plasma sheath, Bohm force scaling in nanoscale plasma, Townsend avalanche pre-ionization model, Paschen-law atmospheric breakdown constraint, plasma propulsion feasibility inequalities, superconducting magnetic energy storage for propulsion, pulse-power plasma acceleration framework, control-volume thrust formulation for plasma actuator, simulation scaffold for electrodeless plasma thruster, plasma physics, computational plasma physics, plasma simulation, multiphysics modeling, drift-diffusion model, electron transport coefficients, Boltzmann solver, electron energy distribution function, EEDF, reduced electric field, E/N, ion mobility, electron mobility, electrical conductivity, magnetic Reynolds number, Lundquist number, Debye length, plasma frequency, skin depth, Hall parameter, Hall effect, magnetic tensor, anisotropic conductivity, Ginzburg-Landau theory, London penetration depth, critical current density, upper critical field, Pauli limit, flux quantum, superconducting coil, superconducting magnet, HTS coil, REBCO, Bi-2212, MgB2, cryogenic engineering, quench protection, magnetic pressure, structural stress, Maxwell stress tensor, control volume, thrust balance, momentum exchange, plasma thruster, electroaerodynamic thruster, corona discharge, corona wind, ozone generation, NOx formation, breakdown voltage, electrical insulation, sheath formation, Bohm criterion, field emission, electron emission, graphene field emitter, carbon nanotube emitter, ADK ionization, tunneling ionization, WKB approximation, plasma dispersion function, Landau damping, Fourier analysis, spectral stability, FDTD, Yee scheme, PIC simulation, particle-in-cell, PIC-MCC, Monte Carlo collisions, constrained transport, divergence cleaning, gauge symmetry, Noether theorem, Lorentz invariants, control allocation, thrust vectoring, aerospace propulsion, future propulsion systems, electric propulsion, electromagnetic propulsion, theoretical framework, feasibility constraints, scaling laws, simulation scaffold, governing equations, closure relations, boundary conditions, sensitivity analysis.
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Aruna Ferdi Wijaya (2026) studied this question.
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