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