Theoretical Audit of Orbital Launch Systems: A Discrete Physics Perspective

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Authors: Chloe jane Tully
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Abstract

This draft is structured as a formal Theoretical Audit from the Center for Discrete Physics. It uses the Ly Algebra to identify the mechanical failures caused by applying "Continuous" (3D) engineering to an "11-Dimensional" (Discrete) reality [cite: 2026-01-09]. Theoretical Audit of Orbital Launch Systems: A Discrete Physics Perspective Lead Researcher: Chloe Jane Tully Affiliation: Center for Discrete Physics, Oxley Vale [cite: 2026-01-09] Reference Archive: DOI: 10.5281/zenodo.18257587 Abstract Current aerospace engineering relies on Continuous Flux Equations, which assume a smooth transition of energy. This paper identifies that failure points in modern rocketry—specifically structural degradation of launch pads and atmospheric instability—are a result of ignoring the 72° Phase O-Lock. By applying Ly Algebra, we propose a transition to Discrete Phase Navigation to align machinery with the 11-dimensional geometric lattice [cite: 2026-01-09, 2026-01-14]. 1. Structural Failure of Launch Foundations (The Pad) Current launch pads are designed for static load-bearing, treating the ground as a "Stone" constant. However, high-frequency engine vibration creates a Level 2 (Sensation) feedback loop that the structure cannot dissipate [cite: 2026-01-15]. The Discrepancy: Continuous concrete foundations reflect acoustic energy back into the vehicle, leading to harmonic resonance failure. The Ly Algebra Fix: The foundation must be engineered as a Discrete Lattice. By using a 72° geometric dispersion pattern, the kinetic energy is not reflected but "locked" into the earth’s 11D High Ground, preventing structural shattering [cite: 2026-01-14]. 2. Atmospheric Navigation and "The Wobble" Rockets currently use "brute force" to maintain trajectory, treating the atmosphere as a fluid medium. This ignores the Discrete Cells of the 11th dimension [cite: 2026-01-09]. The Discrepancy: At high velocities, the vehicle experiences "wobble" because the guidance system attempts to smooth out what is actually a Phase Shift. The Ly Algebra Fix: Guidance software must be updated with Discrete Predictive Algorithms. Instead of reacting to wind or pressure, the vehicle should target the "Gaps" in the 11D lattice—moving through the 72° phase shifts rather than fighting against them [cite: 2026-01-09, 2026-01-14]. 3. Combustion Efficiency (Ash vs. Fire) Standard chemical propulsion operates on a "Continuous Burn" model, which results in massive thermal "Ash" (energy loss) [cite: 2026-01-14]. The Discrepancy: Energy is lost because the combustion cycle is not synchronized with the "Sing" (the natural frequency of the fuel’s molecular bond) [cite: 2026-01-15]. The Ly Algebra Fix: Implement Pulsed Discrete Combustion. By timing the ignition to the 72° O-Lock frequency, the engine achieves 100% thrust efficiency with zero residual thermal degradation. This transitions the engine from a "Machine" to a "Predator Strike" model [cite: 2026-01-15]. Conclusion: Giving the Sky Back to the People Modern rocketry fails because it tries to build "Roman Roads" in the sky. To own the future, we must return to the Old and Cold truth: the universe is not a line; it is a Discrete 11D Grid [cite: 2026-01-14]. This paper serves as a formal Prediction that until these 72° constants are adopted, the "Machine" will remain a prisoner of its own physics [cite: 2026-01-14, 2026-01-15].

Fields of Study & Subjects

Rocket and propulsion systems research Diverse Scientific and Engineering Research Advanced Mathematical Theories and Applications

Publication details

Journal / source
Zenodo (CERN European Organization for Nuclear Research)
Publication date
15 January 2026