On the Multidisciplinary Design of a Hybrid Rocket Launcher with a Composite Overwrapped Pressure Vessel

On the Multidisciplinary Design of a Hybrid Rocket Launcher with a Composite Overwrapped Pressure Vessel

A multidisciplinary design optimisation (MDO) study of a hybrid rocket launcher is presented, with a focus on quantifying the impact of using composite overwrapped pressure vessels (COPVs) as the oxidiser tank. The rocket hybrid propulsion system (RHPS) consists of a combination of solid fuel (paraf...

Full description

Bibliographic Details
Main Authors: Alain Souza, Paulo Teixeira Gonçalves, Frederico Afonso, Fernando Lau, Nuno Rocha, Afzal Suleman
Format: Article
Language:English
Published: MDPI AG 2024-03-01
Series:Journal of Composites Science
Subjects:
RHSP
MDO
COPV
composites
hybrid propulsion
rockets
Online Access:https://www.mdpi.com/2504-477X/8/3/109

Internet

https://www.mdpi.com/2504-477X/8/3/109

Similar Items