The Dewhirst Horizon Relation: Technical Briefing on Post-Relativistic Inertial Modulation and Aerospace Propulsion Optimization

This technical briefing document presents the advanced aerospace, propulsion engineering, and flight navigation applications of the Dewhirst Horizon Relation—a unified scale-invariant physical framework formulated by Richard Stephen Dewhirst. The core mathematical architecture replaces the traditional static speed of light squared velocity constant (c²) with a dynamic, epoch-dependent spacetime horizon coupling parameter called the Dewhirst Coefficient (\(\Omega _{D}\)). By evaluating mass-energy equivalence under variable macro-to-micro cosmic boundaries, this paper outlines two critical commercial and defense applications for advanced research teams: Mitigating the Tsiolkovsky Propellant Penalty: A formal engineering derivation demonstrating that effective localized inertial mass is bound to global cosmic boundary filters rather than being an immutable local constant. The text shows how high-frequency electromagnetic resonance drives can be utilized to artificially modulate the localized quantum temporal fraction surrounding a vehicle's primary hull. This process suppresses local inertial drag, effectively reducing the kinetic force required for high-velocity acceleration and significantly altering traditional rocket propellant mass-fraction calculations. Autonomous Interstellar Navigation Control: A corrected navigation coordinate algorithm for deep-space tracking systems. past heliospheric boundaries. By natively incorporating the Dewhirst background geometric drag vector (8.56 × 10⁻¹⁰ m/s²), automated flight guidance computers can chart ultra-precise trajectories past the 20 AU solar boundary frontier without experiencing unpredicted coordinate drift or requiring auxiliary propellant corrections. To establish absolute mathematical integrity before aerospace review boards, this briefing outlines our complete empirical validation matrix, demonstrating perfect concordance against verified laboratory and astronomical datasets—including CERN LHC particle mass peaks, ESA Gaia stellar velocity plateaus, NASA JPL telemetry logs, and ESA Planck Satellite CMB maps—using only observed baryonic configurations.

Authors

Publication Details

Journal
Zenodo (CERN European Organization for Nuclear Research)
Published
2026-08-24
DOI
https://doi.org/10.5281/zenodo.22073143
Primary Topic
Spacecraft Dynamics and Control
Type
preprint
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The Dewhirst Horizon Relation: Technical Briefing on Post-Relativistic Inertial Modulation and Aerospace Propulsion Optimization

Richard Dewhirst Dewhirst
Zenodo (CERN European Organization for Nuclear Research)
Spacecraft Dynamics and Control
preprint

The Dewhirst Horizon Relation: Technical Briefing on Post-Relativistic Inertial Modulation and Aerospace Propulsion Optimization

Richard Dewhirst Dewhirst
preprint en

Abstract

This technical briefing document presents the advanced aerospace, propulsion engineering, and flight navigation applications of the Dewhirst Horizon Relation—a unified scale-invariant physical framework formulated by Richard Stephen Dewhirst. The core mathematical architecture replaces the traditional static speed of light squared velocity constant (c²) with a dynamic, epoch-dependent spacetime horizon coupling parameter called the Dewhirst Coefficient (\(\Omega _{D}\)). By evaluating mass-energy equivalence under variable macro-to-micro cosmic boundaries, this paper outlines two critical commercial and defense applications for advanced research teams: Mitigating the Tsiolkovsky Propellant Penalty: A formal engineering derivation demonstrating that effective localized inertial mass is bound to global cosmic boundary filters rather than being an immutable local constant. The text shows how high-frequency electromagnetic resonance drives can be utilized to artificially modulate the localized quantum temporal fraction surrounding a vehicle's primary hull. This process suppresses local inertial drag, effectively reducing the kinetic force required for high-velocity acceleration and significantly altering traditional rocket propellant mass-fraction calculations. Autonomous Interstellar Navigation Control: A corrected navigation coordinate algorithm for deep-space tracking systems. past heliospheric boundaries. By natively incorporating the Dewhirst background geometric drag vector (8.56 × 10⁻¹⁰ m/s²), automated flight guidance computers can chart ultra-precise trajectories past the 20 AU solar boundary frontier without experiencing unpredicted coordinate drift or requiring auxiliary propellant corrections. To establish absolute mathematical integrity before aerospace review boards, this briefing outlines our complete empirical validation matrix, demonstrating perfect concordance against verified laboratory and astronomical datasets—including CERN LHC particle mass peaks, ESA Gaia stellar velocity plateaus, NASA JPL telemetry logs, and ESA Planck Satellite CMB maps—using only observed baryonic configurations.

Zenodo (CERN European Organization for Nuclear Research)
Spacecraft Dynamics and Control
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The Dewhirst Horizon Relation: Technical Briefing on Post-Relativistic Inertial Modulation and Aerospace Propulsion Optimization — Richard Dewhirst Dewhirst · Zenodo (CERN European Organization for Nuclear Research) (2026) | TGRS Research Map | TGRS