the more efficent way for rockets

Figshare 2026 Dataset Open access

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Authors: Jonah Mushkatel
DOI: 10.6084/m9.figshare.31441135
Cited by: 0

Abstract

This research proposes a shift in aerospace propulsion design from traditional Parabolic (Quadratic) nozzle geometries () to High-Order Polynomial (Trinomial) structures ().

Fields of Study & Subjects

Rocket and propulsion systems research Computational Fluid Dynamics and Aerodynamics Advanced Aircraft Design and Technologies

Publication details

Journal / source
Figshare
Publication date
1 March 2026
Language
EN
Document type
Dataset