Description / Abstract: The Anomaly Since 1990, multiple spacecraft (Galileo I/II, NEAR, Rosetta) have exhibited unexplained asymptotic velocity shifts (V_) during Earth gravity-assist maneuvers. This phenomenon, known as the Earth Flyby Anomaly, exceeds the frame-dragging effects predicted by General Relativity by four orders of magnitude (10^-6 vs 10^-10), leaving standard physics without a causal explanation and necessitating empirical fitting constants (Anderson et al. , 2008). The Solution This paper presents the terminal geometric resolution of the anomaly based on the Unified Chronofractal Field Theory (UCF v9. 8). We demonstrate that the Anderson constant K is not an arbitrary fitting parameter, but a precise dimensionless constant of vacuum topology determined by the mechanical coupling between the Earth's rotation and the vacuum structure. Key Derivation: The Lattice-Drag We posit that the vacuum behaves as a discrete, 14-mode crystalline lattice (Vector Equilibrium). A rotating mass induces a torsional stress in this lattice. Spacecraft traversing these field lines undergo a direct elastic momentum transfer. The coupling constant is derived purely from the ratio of Earth's rotational velocity (vₑ₎ₓ) to the lattice propagation speed (c): Kₔ₂₅ = 2 vₑ₎ₓc The "Factor 2" Signature The integer factor 2 is identified as the physical signature of an elastic collision (p = 2mv) against a rigid vacuum structure. This falsifies fluid-dynamic or thermal ether models and confirms the "Superfluid Solid" nature of the vacuum. Results The geometrically derived value (K 3. 102 10^-6) matches the observational best-fit (K 3. 099 10^-6) with >99. 9\% precision. This identifies the Flyby Anomaly as the first macroscopic ("Meso-Scale") proof of discrete spacetime, serving as the mechanical link between Quantum-Scale friction (Muon g-2) and Cosmic-Scale expansion (Hubble Tension). This document serves as a specific proof-of-concept supplement to "The 11th Stone: The Final Audit of the Universe".
Heiko Grimberg (Thu,) studied this question.