Neural Network-Based Optimization of Hybrid Rocket Design for Modular Multistage Launch Vehicle

In this paper, an integrated optimization is carried out to find the optimal hybrid rocket engine design for a modular multistage launch vehicle targeting a 500 km polar circular orbit. A single hybrid rocket engine unit is reused across the whole launch vehicle, with each stage constituted by a clu...

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Detalles Bibliográficos

Principais autores:	Paolo Maria Zolla, Alessandro Zavoli, Mario Tindaro Migliorino, Daniele Bianchi
Formato:	Artigo
Idioma:	Inglês
Publicado:	MDPI AG 2026-04-01
Series:	Aerospace
Assuntos:	hybrid rocket engines machine learning multidisciplinary design green propulsion
Acceso en liña:	https://www.mdpi.com/2226-4310/13/4/374
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