This technical report presents a real-time predictive validation of the Higgs Quantum Gravitational Field Theory (HQGFT) applied to the NASA Artemis II mission. By utilizing high-fidelity state vectors from JPL HORIZONS, we demonstrate a significant geometric divergence between classical orbital mechanics and the HQGFT Master Suction Equation. Key Findings: > 1. Prediction of a logarithmic "Suction Drift" ( (R) ) in the translunar trajectory. 2. Calculation of a 52. 99 km/s Delta-v discrepancy, leading to a projected waste of approximately 26, 000 kg of propellant under the Newtonian model. 3. Identification of critical mission risks due to unmodeled Higgs fluid density. This document serves as an active prediction to be contrasted with official telemetry data on April 3, 2026.
Hurtado et al. (Thu,) studied this question.