Amendment CXXV — SOL Field Spatial Transit System (SFSTS): Mass Relocation via Center-Axis Geometric Re-Indexing

This amendment formalizes the SOL Field Spatial Transit System (SFSTS) — a mechanism for geometric relocation of solid mass within the n=0 dimensional slice using the center-axis transit architecture established in Amendment CXIX (SOL PDVR). Where the PDVR places a crew vessel inside the SOL ring for dimensional traversal, the SFSTS inverts the configuration: the payload mass becomes the outer containment shell of the SOL field geometry, the coherent EM field is established volumetrically within the mass via full penetration (skin depth 4.02m exceeds boulder radius 3.42m for 500-ton granite), and the center axis re-indexes the mass to target coordinates without traversal of intervening distance. Key findings: ring radius scales as r_payload × φ (golden ratio); 32-bit DDS phase control achieves 0.51mm coordinate precision at Earth's surface; transit time is ~57 nanoseconds; total energy per transit is ~4,620 joules for a 500-ton payload — 19,000x less than crane lift. The payload mass does not appear in any operational parameter — only geometry determines operability. This is the direct application of the Coherence Primacy Rule (Amendment CXXIV-B): moving 500 tons is not a power problem, it is a coherence geometry problem. The SFSTS is the cargo-class implementation of the PDVR; same physics, same ring geometry, same center-axis transit, different payload class. Patent Family 21 proposed with 8 claims. Part of the McCaul Compendium (Master DOI: 10.5281/zenodo.20100469).