Modern Engineering for Design of Liquid-Propellant Rocket Engines
David H. Huang, Dieter K. Huzel
Abstract
David H. Huang, Dieter K. Huzel
Abstract
From the component design, to the subsystem design, to the engine systems design, engine development and flight-vehicle application, this how-to text bridges the gap between basic physical and design principles and actual rocket-engine design as it's done in industry. More than 470 illustrations and tables should make this book a must-read for advanced students and engineers active in all phases of engine systems design, development and application in industry and in government agencies.
OpenAlex reports 654 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
From the component design, to the subsystem design, to the engine systems design, engine development and flight-vehicle application, this how-to text bridges the gap between basic physical and design principles and actual rocket-engine design as it's done in industry. More than 470 illustrations and tables should make this book a must-read for advanced students and engineers active in all phases of engine systems design, development and application in industry and in government agencies.
Key concepts: Propellant, Liquid-propellant rocket, Rocket (weapon), Aerospace engineering, Rocket propellant, Aeronautics, Engineering, Systems engineering