Hybrid Rocket Combustion

Hybrid Rocket Combustion This book present an effort toward investigation of the local regression rate, average regression rate through the effect of oxidizer injection pressure. The concept of combustion processes presented in this book is based on Marxmann Hybrid rocket combustion for rubber based fuels. This book includes the coverage of: Flat plate Combustion Model Regression Rate Equation for a Cylindrical Grain Hybrid motor and fuel Fabrications

Autorentext

Mr. Yash Pal obtained his master degree in Aeronautical Engineering in 2011 with a thesis on analysis of regression rate of PVC hybrid fuel in hybrid rocket combustion. His area of research include hybrid rocket combustion.He is the author of numerous scientific publications.