RFT-CRX1 "Phoenix Fang": Catch-Reuse Super Heavy Rocket System for Mars Missions

This repository contains the full technical blueprint, simulation evidence, and operational framework for Phoenix Fang — the world’s first fully reusable Mars rocket system designed under Rendered Frame Theory (RFT). Developed by Liam Grinstead, Phoenix Fang introduces a dual-stage catch-and-reuse vehicle optimized for interplanetary transport, harmonically tuned shielding, and simulation-aware AI trajectory correction. Included in this release: 📄 Masterworks Paper Series (8 Documents) System Overview & Mission Architecture SH-R1 Booster & Catch Recovery System MTUS & RHES Shielding Frameseer AI Navigation Core Physical Construction & Assembly Manual Mission Simulation Results & Frame Corrections Post-Mission Maintenance & RHES Recalibration Launch Platform & ChopstickNet Infrastructure 📈 Supporting Evidence & Visuals Simulation graphs from 2,000 mission loops RHES shielding thermal range, AI correction timing, and fuel efficiency metrics Mission logistics flowchart Infographic of Phoenix Fang system Investment pitch deck (.docx) for partners and aerospace investors

Publication Details

Journal
Zenodo (CERN European Organization for Nuclear Research)
Published
2025-05-31
DOI
https://doi.org/10.5281/zenodo.15561784
Primary Topic
Spacecraft Dynamics and Control
Type
article
Field-Weighted Citation Impact
0.00
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article

RFT-CRX1 "Phoenix Fang": Catch-Reuse Super Heavy Rocket System for Mars Missions

Zenodo (CERN European Organization for Nuclear Research)
Spacecraft Dynamics and Control
article

RFT-CRX1 "Phoenix Fang": Catch-Reuse Super Heavy Rocket System for Mars Missions

article en

Abstract

This repository contains the full technical blueprint, simulation evidence, and operational framework for Phoenix Fang — the world’s first fully reusable Mars rocket system designed under Rendered Frame Theory (RFT). Developed by Liam Grinstead, Phoenix Fang introduces a dual-stage catch-and-reuse vehicle optimized for interplanetary transport, harmonically tuned shielding, and simulation-aware AI trajectory correction. Included in this release: 📄 Masterworks Paper Series (8 Documents) System Overview & Mission Architecture SH-R1 Booster & Catch Recovery System MTUS & RHES Shielding Frameseer AI Navigation Core Physical Construction & Assembly Manual Mission Simulation Results & Frame Corrections Post-Mission Maintenance & RHES Recalibration Launch Platform & ChopstickNet Infrastructure 📈 Supporting Evidence & Visuals Simulation graphs from 2,000 mission loops RHES shielding thermal range, AI correction timing, and fuel efficiency metrics Mission logistics flowchart Infographic of Phoenix Fang system Investment pitch deck (.docx) for partners and aerospace investors

Zenodo (CERN European Organization for Nuclear Research)
Industry, innovation and infrastructure
Openalex Percentile: Top 46%
Spacecraft Dynamics and Control
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RFT-CRX1 "Phoenix Fang": Catch-Reuse Super Heavy Rocket System for Mars Missions · Zenodo (CERN European Organization for Nuclear Research) (2025) | TGRS Research Map | TGRS