Investigation of Combustor and Nozzle Performance in a Hybrid Ducted Rocket Using Boron Carbide-Based Solid Fuel

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Authors: Syed Alay Hashim, A. Afra Arah, Anghan Prit Parashotambhai, Ananshi Arora, Soujanya Narlekar, A. Nisha Preethi, Narendranath Basak
Cited by: 0
References: 10

Fields of Study & Subjects

Rocket and propulsion systems research Combustion and Detonation Processes Computational Fluid Dynamics and Aerodynamics

Publication details

Journal / source
Lecture notes in mechanical engineering
Pages
381–390
Publication date
1 January 2026
Language
EN
Document type
Book chapter