GyroShell: A Rotating Outer Shell Rocket for Drag Reduction, Stability, and Efficiency

A concept proposal for a rocket architecture that uses an independently rotating outer shell to reduce aerodynamic drag, enhance stability, and increase fuel efficiency. Developed independently through fluid dynamics principles, this submission aims to inspire new directions in rocket propulsion and launch optimization.

Publication Details

Journal
Zenodo (CERN European Organization for Nuclear Research)
Published
2025-06-30
DOI
https://doi.org/10.5281/zenodo.15775986
Primary Topic
Rocket and propulsion systems research
Type
article
Field-Weighted Citation Impact
0.00
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article

GyroShell: A Rotating Outer Shell Rocket for Drag Reduction, Stability, and Efficiency

Zenodo (CERN European Organization for Nuclear Research)
Rocket and propulsion systems research
article

GyroShell: A Rotating Outer Shell Rocket for Drag Reduction, Stability, and Efficiency

article en

Abstract

A concept proposal for a rocket architecture that uses an independently rotating outer shell to reduce aerodynamic drag, enhance stability, and increase fuel efficiency. Developed independently through fluid dynamics principles, this submission aims to inspire new directions in rocket propulsion and launch optimization.

Zenodo (CERN European Organization for Nuclear Research)
Affordable and clean energy
Openalex Percentile: Top 43%
Rocket and propulsion systems research
DOIOpen Access PDFOpenAlex
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GyroShell: A Rotating Outer Shell Rocket for Drag Reduction, Stability, and Efficiency · Zenodo (CERN European Organization for Nuclear Research) (2025) | TGRS Research Map | TGRS