Internal Combustion Processes of Liquid Rocket Engines PDF Download
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Author: Zhen-Guo Wang
Publisher: John Wiley & Sons
ISBN: 1118890043
Category : Technology & Engineering
Languages : en
Pages : 396
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Book Description
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.
Author: Zhen-Guo Wang
Publisher: John Wiley & Sons
ISBN: 1118890043
Category : Technology & Engineering
Languages : en
Pages : 396
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Book Description
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.
Author: Darby Burgess Makel
Publisher:
ISBN:
Category :
Languages : en
Pages : 346
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Book Description
Author: Mark L. Dranovsky
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN: 9781563479212
Category : Technology & Engineering
Languages : en
Pages : 352
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Book Description
This is the first book in the literature to cover the development and testing practices for liquid rocket engines in Russia and the former Soviet Union.Combustion instability represents one of the most challenging probelms in the development of propulsion engines. A famous example is the F-1 engines for the first stage of the Saturn V launch vehicles in the Apollo project. More than 2000 full engine tests and a vast number of design modifications were conducted to cure the instability problem.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. It covers more than 50 years of research, with an emphasis placed on the advances made since 1970.The book was prepared by a former R&D director of the Research Institute of Chemical Engineering, NIICHIMMASH, the largest liquid rocket testing center in the world, and has been carefully edited by three well-known experts in the field.
Author: Dieter K. Huzel
Publisher: AIAA
ISBN: 9781600864001
Category : Liquid propellant rocket engines
Languages : en
Pages : 452
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Book Description
Author: Robert H. Goddard
Publisher:
ISBN: 9781494067243
Category :
Languages : en
Pages : 270
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Book Description
This is a new release of the original 1960 edition.
Author: Richard C. Mulready
Publisher: SAE International
ISBN: 9780768006643
Category : Technology & Engineering
Languages : en
Pages : 226
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Book Description
FROM THE PREFACE: This book celebrates the wonderful projects on which we worked at Pratt & Whitney during the almost magical quarter century bounded by World War II and the competition to develop the Space Shuttle engine. Some of the work has never been described until this book because of stringent security classifications that are now lifted. This book is about the almost unbelievable engines and the dedicated group of people who made the engines real. Most of these unique projects were not the daily 'bread and butter' for Pratt & Whitney and thus were free from much of the survival pressure that typically surrounds that work. Instead, they were driven by the challenge of attempting things that had never been done. Two lasting discoveries that came from the work of the group were the RL10 hydrogen rocket engine, which has been used to launch most large satellites over the past half-century, and the development of the technology for the high-pressure staged combustion rocket engine used in the Space Shuttle.CONTENTS INCLUDE: Ramjets - The Early Days at the Research Laboratory; T57 - The Largest Turboprop; Liquid Hydrogen and the 304 Engine - Suntan; RL10 - My Only Moneymaker; High-Pressure Rockets - A Decade and One-Half Billion Dollars; Boost Glide and the XLR129-Mach 20 at 200,000 Feet; XLD-1 Gas Dynamic Laser; The Space Shuttle Engine; A Cry for Help.
Author: DP Mishra
Publisher: CRC Press
ISBN: 1351708414
Category : Technology & Engineering
Languages : en
Pages : 364
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Book Description
The book follows a unified approach to present the basic principles of rocket propulsion in concise and lucid form. This textbook comprises of ten chapters ranging from brief introduction and elements of rocket propulsion, aerothermodynamics to solid, liquid and hybrid propellant rocket engines with chapter on electrical propulsion. Worked out examples are also provided at the end of chapter for understanding uncertainty analysis. This book is designed and developed as an introductory text on the fundamental aspects of rocket propulsion for both undergraduate and graduate students. It is also aimed towards practicing engineers in the field of space engineering. This comprehensive guide also provides adequate problems for audience to understand intricate aspects of rocket propulsion enabling them to design and develop rocket engines for peaceful purposes.
Author: H. J. Ellis
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 156
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Book Description
Author: George Paul Sutton
Publisher: AIAA
ISBN: 9781563476495
Category : Technology & Engineering
Languages : en
Pages : 936
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Book Description
Liquid propellant rocket engines have propelled all the manned space flights, all the space vehicles flying to the planets or deep space, virtually all satellites, and the majority of medium range or intercontinental range ballistic missiles.
Author: National Research Council
Publisher: National Academies Press
ISBN: 0309266564
Category : Science
Languages : en
Pages : 115
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Book Description
On June 15, 2011, the Air Force Space Command established a new vision, mission, and set of goals to ensure continued U.S. dominance in space and cyberspace mission areas. Subsequently, and in coordination with the Air Force Research Laboratory, the Space and Missile Systems Center, and the 14th and 24th Air Forces, the Air Force Space Command identified four long-term science and technology (S&T) challenges critical to meeting these goals. One of these challenges is to provide full-spectrum launch capability at dramatically lower cost, and a reusable booster system (RBS) has been proposed as an approach to meet this challenge. The Air Force Space Command asked the Aeronautics and Space Engineering Board of the National Research Council to conduct an independent review and assessment of the RBS concept prior to considering a continuation of RBS-related activities within the Air Force Research Laboratory portfolio and before initiating a more extensive RBS development program. The committee for the Reusable Booster System: Review and Assessment was formed in response to that request and charged with reviewing and assessing the criteria and assumptions used in the current RBS plans, the cost model methodologies used to fame [frame?] the RBS business case, and the technical maturity and development plans of key elements critical to RBS implementation. The committee consisted of experts not connected with current RBS activities who have significant expertise in launch vehicle design and operation, research and technology development and implementation, space system operations, and cost analysis. The committee solicited and received input on the Air Force launch requirements, the baseline RBS concept, cost models and assessment, and technology readiness. The committee also received input from industry associated with RBS concept, industry independent of the RBS concept, and propulsion system providers which is summarized in Reusable Booster System: Review and Assessment.
