Journal of Space Exploration, Propulsion and Aerospace Systems
Novel Space Propulsion System Based on Cosmic Energy Inversion (CEIT) Theory
Abstract
Ashour Ghelichi
An updated theoretical framework for propellant less geometric propulsion is presented, based on the Cosmic Energy Inversion Theory (CEIT-v4). This work extends the earlier preprint (2025, v2) by introducing three major refinements: (1) a precise and operational definition of the local field reference Δ�?�(�?�) = �?�int(�?�) − �?�local(�?�spacecraft, �?�), establishing that thrust is always measured relative to the instantaneous ambient field at the spacecraft's position; (2) a hierarchical navigation protocol with a domain-exit condition �??∇�?�current(�?�boundary)�?? = �??∇�?�larger(�?�boundary)�?? for transitions between planetary, stellar, galactic, and intergalactic scales; and (3) an examination of momentum conservation via the contracted Bianchi identity , suggesting that reaction momentum is absorbed as propagating torsion disturbances in the ambient gradient structure. A system architecture is proposed comprising a primary sphere for main thrust generation and crew inertial isolation (∇�?�core = 0), along with secondary spheres for attitude control. Detailed numerical mission analysis has been deliberately deferred to future work following independent parameter calibration. All results remain theoretical and require independent calibration and experimental verification. This paper is offered as a starting point for future research and as a roadmap for the potential development of geometric propulsion technology.