17.1 N₂O-Based Systems 17.2 High-Concentration H₂O₂ 17.3 Non-Toxic Oxidizers and Low-Emissions Fuels
3.1 Oxidizers (LOX, N₂O, H₂O₂, N₂O₄) 3.2 Fuels (HTPB, PMMA, Paraffin, ABS, Hybrid Nanomaterials) 3.3 Equilibrium Combustion and Adiabatic Flame Temperature 3.4 Mixture Ratio and Its Effect on Performance 3.5 Combustion Products and Environmental Impact Part II: Internal Ballistics and Combustion Physics Chapter 4: Fuel Regression Rate 4.1 Classical Boundary-Layer Combustion Theory 4.2 Diffusion Flame Mechanism 4.3 Empirical Regression Rate Laws 4.4 Classical Low-Rate Problem and Its Implications the science and design of the hybrid rocket engine pdf
16.1 Metalized and Nano-Enhanced Fuels 16.2 Hybrid Boosters for Launch Vehicles 16.3 High-Pressure Hybrid Engines N₂O₄) 3.2 Fuels (HTPB
14.1 Multidisciplinary Optimization (Mass, Performance, Cost) 14.2 Trade-offs: Regression Rate vs. Structural Mass 14.3 Throttling Strategy Optimization 14.4 Case Study: Small Sounding Rocket Part V: Advanced Topics and Future Directions Chapter 15: Additive Manufacturing for Hybrid Rockets 15.1 3D-Printed Fuel Grains with Complex Ports 15.2 Embedded Oxidizer and Controlled Porosity 15.3 Rapid Prototyping for Test-Fire Iterations the science and design of the hybrid rocket engine pdf
It is structured to progress from fundamental theory to practical design, manufacturing, testing, and advanced topics. Foreword Preface Acknowledgments Nomenclature Part I: Foundations of Hybrid Rocket Propulsion Chapter 1: Introduction to Hybrid Rockets 1.1 Historical Development 1.2 Basic Hybrid Rocket Configuration 1.3 Comparison with Solid and Liquid Engines 1.4 Advantages and Challenges 1.5 Key Applications (sounding rockets, space tourism, upper stages)