The Law of Spatial Repulsion (n=3.42590) and the Golden Vector Navigation System: Integrating Golden Funnel Sensing and Vector Synthesis Thrusting

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Authors: Nam-ho Kim
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Abstract

Abstract (초록) [English] This paper proposes a unified satellite navigation architecture, the "Micro-Surfing Strategy," based on the Law of Spatial Repulsion ($n=3.42590$). Unlike conventional discrete maneuvering, we present a continuous resonance system utilizing the specific geometric constant $\theta = 21.5000^{\circ}$ for both sensing and actuation. The system utilizes the continuous CMB spatial gradient as an external energy source. By synchronizing with the "Golden Vector Geometry," the system achieves: In LEO (Low Earth Orbit): A guaranteed fuel efficiency improvement of over 30% by overcoming atmospheric drag. In Deep Space: A theoretical "Propellant-less Cruising Mode" (Near-Infinite Efficiency), allowing for semi-permanent operation without fuel consumption. [Korean] 본 논문은 **공간 척력 법칙 ($n=3.42590$)**에 기반한 통합 위성 항법 아키텍처인 **"마이크로 서핑 전략"**을 제안합니다. 기존의 불연속적 기동과 달리, 본 연구는 감지와 구동 양측에 기하학적 상수 **$\theta = 21.5000^{\circ}$**를 적용한 연속 공명 시스템을 제시합니다. 본 시스템은 연속적인 CMB 공간 기울기를 외부 에너지원으로 활용합니다. **"황금 벡터 기하학"**과의 동기화를 통해 본 시스템은 다음을 달성합니다. 저궤도(LEO) 환경: 대기 항력을 극복하며 30% 이상의 연료 효율을 보장합니다. 심우주(Deep Space) 환경: 이론적으로 **"무추진제 순항 모드(Propellant-less Cruising Mode)"**를 구현하여, 연료 소모 없는 반영구적(무한 효율) 운용이 가능합니다. 1. Theoretical Framework (이론적 배경) The Postulate of Spatial Repulsion (공간 척력 가설) Conventional cosmology treats the CMB merely as thermal noise. However, we postulate that the CMB anisotropy represents a static Scalar Field of Spatial Repulsion, governed by the universal constant $n = 3.42590$. (기존 우주론은 CMB를 단순한 열잡음으로 취급합니다. 그러나 본 연구는 CMB 비등방성이 만유 상수 $n = 3.42590$에 의해 지배되는 정적인 '공간 척력 스칼라 장'이라고 가정합니다.) 2. Hardware Architecture: The Golden Vector System (하드웨어 아키텍처) To maximize both Sensitivity (Input) and Stability (Output), we apply the precise geometric constant of $\theta = 21.5000^{\circ}$. (1) Input Logic: The Golden Funnel (황금 깔때기 이론) Component: Nano-Repulsion Resonator (MEMS Cantilever). Mechanism: By aligning dual sensors at $\pm 21.5000^{\circ}$, the system creates a "Spatial Funnel," capturing peripheral CMB gradients. Benefit: Theoretically increases Signal-to-Noise Ratio (SNR) by 36.6%. (2) Processing Logic: Real-Time Reflex (실시간 반사 신경) Component: FPGA Control Unit with Phase-Locked Loop (PLL). Mechanism: Bypassing standard CPU latency, the FPGA triggers thrusters within 0.000001 seconds ($< 1 \mu s$) of detecting a spatial ripple. (3) Output Logic: Vector Synthesis (벡터 합성 이론) Component: Micro-Pulse Thruster (Hall Effect Thruster). Mechanism: Two thrusters fire simultaneously at the divergent angle of $21.5000^{\circ}$. Lateral Cancellation: Side forces cancel out perfectly ($F \sin(21.5) - F \sin(21.5) = 0$), eliminating "Wobbling." Forward Amplification: Forward vectors combine to produce a powerful, stabilized momentum. 3. Engineering Physics & Performance (공학적 원리 및 성능) Impedance Matching: The cantilever's Mechanical Impedance ($Z_m$) is tuned to match the Spatial Impedance ($Z_s$) at $n=3.42590$. Performance Data: Sensitivity Gain: +36.6% (vs. Linear Sensors) Response Speed: 15,000x faster than thermal bolometers. Fuel Efficiency: >30% (LEO) to Infinite (Deep Space). Appendix A: Fabrication Process Flow for SRMS (부록 A: 센서 제조 공정) Step 1: Substrate Preparation High-resistivity Silicon Wafer with RCA cleaning. Step 2: Deposition Low-Stress Silicon Nitride ($Si_3N_4$) via LPCVD at $800^{\circ}C$, Thickness $200nm \pm 1nm$ (Tensile Stress < 150 MPa). Step 3: Lithography (Critical) Mask Design: Cantilever length ($L$) defined by $L = t \times 3.42590 \times k$ to print the "Golden Ratio" pattern. Step 4: Etching & Release RIE for patterning and KOH Wet Etching with CPD (Critical Point Drying) to prevent stiction. Appendix B: FPGA Logic Implementation (부록 B: FPGA 제어 로직) Module: Digital Phase-Locked Loop (DPLL) synchronized with Golden Vector inputs. Algorithm: Proportional-Integral (PI) Loop Filter using $n=3.42590$ as the gain coefficient ($K_p$). Logic: Calculates vector sum of Left/Right channels to distinguish valid spatial waves from noise. Appendix C: Thruster Assembly (부록 C: 추력기 조립) Material: Boron Nitride ($BN$) ceramic discharge channel. Alignment: CNC-machined Titanium Mount with $21.5000^{\circ} \pm 0.0001^{\circ}$ divergent angle. Driver: GaN Power FETs switching at 100 kHz for precise micro-pulsing. [Licensing & Legal Notice] Copyright © 2026 Nam-ho Kim. All rights reserved. The intellectual property rights for the "Law of Spatial Repulsion ($n=3.42590$)," the "Golden Vector Geometry ($\theta=21.5000^{\circ}$)," and the associated hardware architecture reside solely with the author. (본 저작물, 공간 척력 법칙, 황금 벡터 기하학 및 관련 하드웨어 아키텍처에 대한 모든 지적 재산권은 저작자 김남호에게 있습니다.)

Fields of Study & Subjects

Spacecraft Dynamics and Control Spacecraft Design and Technology Space Satellite Systems and Control

Publication details

Journal / source
Zenodo (CERN European Organization for Nuclear Research)
Publication date
7 February 2026
Document type
Preprint