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Liquid Rocket Thrust Chambers
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Author :Vigor Yang Publisher :AIAA (American Institute of Aeronautics & Astronautics) ISBN 13 : Total Pages :776 pages Book Rating :4.3/5 (91 download)
Book Synopsis Liquid Rocket Thrust Chambers by : Vigor Yang
Download or read book Liquid Rocket Thrust Chambers written by Vigor Yang and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 2004 with total page 776 pages. Available in PDF, EPUB and Kindle. Book excerpt: This is the first major publication on liquid-rocket combustion devices since 1960, and includes 20 chapters prepared by world-renowned experts. Each chapter focuses on a specific aspect of liquid-propellant combustion and thrust chamber dynamics, and is incorporated into the volume in a well-organized, cohesive manner. There are contributions from nine different countriesChina, France, Germany, Italy, Japan, the Netherlands, Russia, Sweden, and the United States.
Book Synopsis Progress In Astronautics and Aeronautics by : Mohammed Habiballah
Download or read book Progress In Astronautics and Aeronautics written by Mohammed Habiballah and published by AIAA. This book was released on 2004 with total page 784 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Liquid Rocket Engine by : Rene Nardi Rezende
Download or read book Liquid Rocket Engine written by Rene Nardi Rezende and published by SAE International. This book was released on 2018-11-15 with total page 158 pages. Available in PDF, EPUB and Kindle. Book excerpt: The great engineering achievement required to overcome most of the challenges and obstacles that prevented turning rocket design from art into science took place in Europe and the United States between the 1930s and the 1950s. With the vast majority of the engines currently in operation developed in the “pre-computer” age, there are new opportunities to update the design methodologies using technology that can now handle highly complex calculations fast. The space sector with an intense focus on efficiency is driving the need for updating, adapting or replacing the old modeling practices with new tools capable of reducing the volume of resources and the time required to complete simulations and analysis. This book presents an innovative parametric model applicable to the project of some elements of the liquid rocket thrust chamber with the level of detail and accuracy appropriate to the preliminary design phase. It addresses the operating characteristics and dimensioning of some thrust chamber elements through a set of equations and parameters, which include thrust or propellant characteristics. The model degree of sophistication was adjusted to the requirements of the Project Life Cycle Phase B, while also enabling quick analysis of new configurations from changes in initial project parameters.
Book Synopsis Liquid Rocket Engine Combustion Instability by : Vigor Young
Download or read book Liquid Rocket Engine Combustion Instability written by Vigor Young and published by AIAA. This book was released on 1995 with total page 606 pages. Available in PDF, EPUB and Kindle. Book excerpt: Annotation Since the invention of the V-2 rocket during World War II, combustion instabilities have been recognized as one of the most difficult problems in the development of liquid propellant rocket engines. This book is the first published in the United States on the subject since NASA's Liquid Rocket Combustion Instability (NASA SP-194) in 1972. In this book, experts cover four major subject areas: engine phenomenology and case studies, fundamental mechanisms of combustion instability, combustion instability analysis, and engine and component testing. Especially noteworthy is the inclusion of technical information from Russia and China--a first.
Book Synopsis History of Liquid Propellant Rocket Engines by : George Paul Sutton
Download or read book History of Liquid Propellant Rocket Engines written by George Paul Sutton and published by AIAA. This book was released on 2006 with total page 936 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Liquid Rocket Engine Thrust Chamber by : Rene Nardi Rezende
Download or read book Liquid Rocket Engine Thrust Chamber written by Rene Nardi Rezende and published by . This book was released on 2018 with total page 158 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book presents an innovative parametric model applicable to the project of some elements of the liquid rocket thrust chamber with the level of detail and accuracy appropriate to the preliminary design phase. It addresses the operating characteristics and dimensioning of some thrust chamber elements through a set of equations and parameters, which include thrust or propellant characteristics. The model degree of sophistication was adjusted to the requirements of the Project Life Cycle Phase B, while also enabling quick analysis of new configurations from changes in initial project parameters.
Book Synopsis Modern Engineering for Design of Liquid-Propellant Rocket Engines by : Dieter K. Huzel
Download or read book Modern Engineering for Design of Liquid-Propellant Rocket Engines written by Dieter K. Huzel and published by AIAA. This book was released on 1992 with total page 452 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Liquid Propellant Rocket Combustion Instability by : David T. Harrje
Download or read book Liquid Propellant Rocket Combustion Instability written by David T. Harrje and published by . This book was released on 1972 with total page 674 pages. Available in PDF, EPUB and Kindle. Book excerpt: The solution of problems of combustion instability for more effective communication between the various workers in this field is considered. The extent of combustion instability problems in liquid propellant rocket engines and recommendations for their solution are discussed. The most significant developments, both theoretical and experimental, are presented, with emphasis on fundamental principles and relationships between alternative approaches.
Book Synopsis Liquid Propellant Rocket Combustion Instability by :
Download or read book Liquid Propellant Rocket Combustion Instability written by and published by . This book was released on 1972 with total page 668 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :Mark L. Dranovsky Publisher :AIAA (American Institute of Aeronautics & Astronautics) ISBN 13 :9781563479212 Total Pages :352 pages Book Rating :4.4/5 (792 download)
Book Synopsis Combustion Instabilities in Liquid Rocket Engines by : Mark L. Dranovsky
Download or read book Combustion Instabilities in Liquid Rocket Engines written by Mark L. Dranovsky and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 2007 with total page 352 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Liquid Rocket and Propellants by : L.E. Bollinger
Download or read book Liquid Rocket and Propellants written by L.E. Bollinger and published by Elsevier. This book was released on 1960 with total page 698 pages. Available in PDF, EPUB and Kindle. Book excerpt: Liquid Rocket and Propellants
Book Synopsis Theoretical Performance of Hydrogen-oxygen Rocket Thrust Chambers by : Gilbert K. Sievers
Download or read book Theoretical Performance of Hydrogen-oxygen Rocket Thrust Chambers written by Gilbert K. Sievers and published by . This book was released on 1961 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt: Theoretical rocket performance data for the propellant combination of liquid hydrogen and liquid oxygen are presented in convenient graphical forms to permit rapid determination of specific impulse, vacuum specific impulse, and characteristic velocity. Data are presented for both frozen and equilibrium composition during expansion for chamber pressures of 15, 30, 60, 150, 300, 600, 900 and 1200 pounds per square inch absolute over a wide range of percent fuel from approximately 8 to 34 and area ratios to approximately 300. For rapid calculation of the theoretical nozzle performance with over- or under- expansion, separated flow, and introduction of propellants at different initial conditions or heat loss from the combustion chamber, the following theoretical data are also presented: combustion-chamber temperature, nozzle-exit temperature, and the ratio of chamber-pressure to nozzle-exit pressure. An easy method is given for estimating theoretical specific impulse at chamber pressures other than those presented.
Book Synopsis Fabrication of Liquid-rocket Thrust Chambers by Electroforming by : Rudolph A. Duscha
Download or read book Fabrication of Liquid-rocket Thrust Chambers by Electroforming written by Rudolph A. Duscha and published by . This book was released on 1974 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A High-performance 250-pound-thrust Rocket Engine Utilizing Coaxial-flow Injection of JP-4 Fuel and Liquid Oxygen by : Samuel Stein
Download or read book A High-performance 250-pound-thrust Rocket Engine Utilizing Coaxial-flow Injection of JP-4 Fuel and Liquid Oxygen written by Samuel Stein and published by . This book was released on 1959 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Rocket Propulsion Elements by : George Paul Sutton
Download or read book Rocket Propulsion Elements written by George Paul Sutton and published by Wiley-Interscience. This book was released on 1976 with total page 584 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Rocket Propulsion Elements by : George Paul Sutton
Download or read book Rocket Propulsion Elements written by George Paul Sutton and published by Wiley-Interscience. This book was released on 1986 with total page 392 pages. Available in PDF, EPUB and Kindle. Book excerpt: A revision of the standard text on the basic technology, performance and design rationale of rocket propulsion. After discussing fundamentals, such as nozzle thermodynamics, heat transfer, flight performance and chemical reaction analysis, the book continues with treatments of various types of liquid and solid propellants and rocket testing. It brings together the engineering science disciplines necessary for rocket design: thermodynamics, heat transfer, flight mechanics, chemical reactions and materials behavior. SI units and information on computer-aided testing have also been added.
Book Synopsis Some Factors Influencing Heat Transfer to Liquid-propellant Rocket-thrust-chamber Coolant Channels by : Roger C. Krueger
Download or read book Some Factors Influencing Heat Transfer to Liquid-propellant Rocket-thrust-chamber Coolant Channels written by Roger C. Krueger and published by . This book was released on 1966 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
