(Ⅻ)Theoretical Deduction and Prototype Analysis of Field Dynamic Thruster

Description This work presents the theoretical deduction and prototype analysis of a field dynamic thruster, a new propulsion device based on AI field modulation and electromagnetic energy conversion. Different from traditional chemical and jet propulsion, the thruster generates directional thrust by dynamically regulating electromagnetic field distribution, without relying on fuel or reaction mass. The paper establishes a mathematical model of field force coupling, derives the thrust generation mechanism under multi-physical field interaction, and completes the structural design and control logic of a small-scale prototype. Through simulation and bench testing, the field response characteristics, energy conversion efficiency, and thrust output performance are verified. The results show that the field dynamic thruster has the advantages of low energy consumption, no pollution, long service life, and strong environmental adaptability. It can be applied to near-space vehicles, low-orbit satellites, deep-space probes, and interstellar exploration platforms, providing a new theoretical and technical basis for future high-efficiency, sustainable space propulsion systems.