This record establishes a firmware-only solution for the suppression of destructive acoustic resonance in the Starship thrust puck assembly. By implementing a Phase-Conjugate Fuel-Pulse (H^*) within the Flight Control System (FCS), the engine matching logic treats the combustion manifold as a Self-Adjoint operator. This allows for the real-time neutralization of harmonic coupling between Raptor engines, eliminating vibration-induced stress without additional mass-based dampening or hardware shielding.
James Rider (Thu,) studied this question.