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Modern Engineering For Design Of Liquid Propellant Rocket Engines

Author: Dieter K. Huzel
Publisher: Aiaa
ISBN: 9781563470134
Size: 35.58 MB
Format: PDF
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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 its done in industry. More than 470 illustrations and tables help to 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.

History Of Liquid Propellant Rocket Engines

Author: George Paul Sutton
Publisher: AIAA
ISBN: 9781563476495
Size: 16.84 MB
Format: PDF, Mobi
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Written by a rocket propulsion expert, this book gives an account of the liquid propellant rocket engine field. It includes information on the early pioneers, amateur rocket societies, evolution of hardware components, investigations of different liquid propellants, and the principal areas of application.

Rocket Propulsion Elements

Author: George P. Sutton
Publisher: John Wiley & Sons
ISBN: 1118753917
Size: 51.24 MB
Format: PDF, ePub, Mobi
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THE DEFINITIVE INTRODUCTION TO ROCKET PROPULSION THEORY AND APPLICATIONS The recent upsurge in global government and private spending and in space flight events has resulted in many novel applications of rocket propulsion technology. Rocket Propulsion Elements remains the definitive guide to the field, providing a comprehensive introduction to essential concepts and applications. Led by industry veteran George P. Sutton and by Professor Oscar Biblarz, this book provides interdisciplinary coverage including thermodynamics, aerodynamics, flight performance, propellant chemistry and more. This thoroughly revised ninth edition includes discussion and analysis of recent advances in the field, representing an authoritative reference for students and working engineers alike. In any engineering field, theory is only as useful as it is practical; this book emphasizes relevant real-world applications of fundamental concepts to link "thinking" and "doing". This book will help readers: Understand the physics of flight and the chemistry of propulsion Analyze liquid, solid, gas, and hybrid propellants, and the engines they fuel Consider high-temperature combustion, stability, and the principles of electric and chemical propulsion Dissect the workings of systems in common use around the world today Delve into the latest advances in materials, systems, propellants, and more Broad in scope, rich in detail, and clear in explanation, this seminal work provides an unparalleled foundation in aerospace engineering topics. Learning through the lens of modern applications untangles complex topics and helps students fully grasp the intricacies on a more intuitive level. Rocket Propulsion Elements, Ninth Edition merges information and utility building a solid foundation for innovation.

Combustion Instabilities In Liquid Rocket Engines

Author: Mark L. Dranovsky
Publisher: Amer Inst of Aeronautics &
ISBN: 9781563479212
Size: 65.64 MB
Format: PDF, Mobi
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Covers the development and testing practices for liquid rocket engines in Russia and the former Soviet Union. This book contains first-hand information about the testing and development practices for treating liquid rocket combustion-instability problems in Russia and the former Soviet Union.

From Peenem Nde To Canaveral

Author: Dieter Huzel
Publisher: Pickle Partners Publishing
ISBN: 1782898697
Size: 62.65 MB
Format: PDF, Kindle
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Dieter Huzel was an electronic engineer with his whole career ahead of him when Germany lurched into the Second World War, he was conscripted and destined for the Russian Front when fate intervened. He and many other scientists were re-assigned from combat duty to the top secret installation at Peenemünde Island off the Baltic coast as part of the Nazi search for “Wonder Weapons”. Huzel describes how he became an integral part of the V weapon program which, despite the frequent Allied bombings, produced the feared V-1 and V-2 rockets that rained down on liberated parts of Europe during the later years of the war. As the tide turned against the Nazi regime, Huzel tells of the shifts in production of these weapons to central Germany and his team’s rising fear that the rocket technology would fall into the hands of the Russians. However, Huzel and his team were captured by the West and offered re-location to Britain or America. Huzel and his former director, Werner Von Braun, opted for America where they would become part of the ground-breaking Rocketdyne research team and spearhead of the NASA push for space exploration.

The Science And Design Of The Hybrid Rocket Engine

Author: Richard M. Newlands
Publisher: Lulu Press, Inc
ISBN: 0244902917
Size: 67.66 MB
Format: PDF, ePub, Docs
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This is a textbook about rocket engineering, concentrating on the nitrous oxide hybrid rocket engine, both small and large. It’s also a book about the science of chemical rockets in detail: three of the chapters are full of in-depth rocket science describing how all chemical rockets work. After a first chapter brushing up on the science and maths you’ll need, the book describes the choice and safe use of hybrid rocket propellants, and how they’re handled in practice. Then there are the rocket science chapters. Then you learn how to design, construct, and operate, a large hybrid rocket engine capable of getting you into Space. The book also includes a practical guide to the testing of hybrid rocket engines large and small, and how to fly them safely. Included are full instructions for programming a rocket trajectory simulator in Microsoft Excel, and several appendices containing rocketry information and equations, and instructions on how to design a bell nozzle.

Internal Combustion Processes Of Liquid Rocket Engines

Author: Zhen-Guo Wang
Publisher: John Wiley & Sons
ISBN: 1118890051
Size: 48.73 MB
Format: PDF, Mobi
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This book concentrates on modeling and numerical simulations of combustion in liquid rocket engines, covering liquid propellant atomization, evaporation of liquid droplets, turbulent flows, turbulent combustion, heat transfer, and combustion instability. It presents some state of the art models and numerical methodologies in this area. The book can be categorized into two parts. Part 1 describes the modeling for each subtopic of the combustion process in the liquid rocket engines. Part 2 presents detailed numerical methodology and several representative applications in simulations of rocket engine combustion.