Acceleration Reality, Δf Elasticity, and Resonant Drive: A Classical-Compatible Mechanism Layer in USP Field Theory
Year: 2025
Type: article
Abstract: The Falcon Strider (SR-FS1) is a compact four-person hybrid aerospace vehicle designed for atmospheric and orbital operations using a three-stage propulsion system. This mission profile outlines a retrograde (east-to-west) launch followed by a prograde (west-to-east) return, allowing for precise orbital targeting and efficient atmospheric reentry using USP Field Theory principles. Key innovations: Continuous engine overlap: Jet, ramjet, and field compression engines remain partially active together to ensure stability throughout all flight phases. Minimum acceleration approach: Ensures safety and control while transitioning through multiple flight environments. Dual-turn return maneuver: Utilizes Earth’s spin and USP field dynamics to re-enter smoothly with minimal energy. The package includes a mission overview document, a labeled engine cutaway diagram, a procedural launch chart, and a flight trajectory map.
Author: Sepehri, Sadegh
Language: English
Subfield: Astronomy and Astrophysics
Field: Physics and Astronomy
Domain: Physical Sciences
Open Access status: green
OpenAlex ID: W6893422636
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