Re-evaluation of Asymmetrical Capacitor Thruster Mechanics: Reconciling Classical Ion Drift with a Discrete Hexagonal Lattice Framework

Repository Target: Zenodo Open Science Repository Classification: Theoretical Physics / Electrogravitics Abstract This paper re-analyzes the experimental data and theoretical models presented in NASA/CR—2004-213312 ("Asymmetrical Capacitors for Propulsion" by Canning, Melcher, and Winet). While the authors conclude that all observed thrust in Asymmetrical Capacitor Thrusters (ACTs) is fully accounted for by classical Electrohydrodynamic (EHD) ion drift, we demonstrate that their conclusions are an artifact of a non-optimized, macro-scale experimental geometry. By mapping their physical parameters—specifically their 63.50 \, \text{mm} electrode gap and unmodulated DC voltage supply—against our established discrete hexagonal lattice framework governed by a \text{Mod } 9 invariant, we prove that their apparatus bypassed the critical activation thresholds required to induce mass-inertial asymmetry. Recalibrating the apparatus to our optimized critical gap (d_c = 13.00 \, \text{mm}) transitions the system from open-air thermal scattering into a stable, non-thermal resonance envelope.