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Droplet Vaporization/Combustion Stability-Based Design of Pre-Combustion Chambers for Hybrid Propellant Rocket Motors

Hybrid Propellant Rocket Motors (HPRMs) have been advancing rapidly in recent years. These improvements are finally increasing their competitiveness in the global launch-vehicle market. However, some topics, such as the pre-combustion chamber design, still require more in-depth studies. Few studies...

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Principais autores: Maurício Sá Gontijo, Olexiy Shynkarenko, Artur E. M. Bertoldi
Format: Artigo
Sprog:Inglês
Udgivet: MDPI AG 2025-06-01
Serier:Energies
Fag:
hybrid propellant rocket motor
pre-combustion chamber
droplet vaporization
combustion instability
Online adgang:https://www.mdpi.com/1996-1073/18/12/3123
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