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Theory And Calculation Of Feed Units Of Liquid Propellant Rocket Engines
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Book Synopsis Theory and Calculation of Feed Units of Liquid-Propellant Rocket Engines by : B. V. Ovsyannikov
Download or read book Theory and Calculation of Feed Units of Liquid-Propellant Rocket Engines written by B. V. Ovsyannikov and published by . This book was released on 1973 with total page 793 pages. Available in PDF, EPUB and Kindle. Book excerpt: In the book information on the theory and hydraulic design of pumps and turbines of turbopump units (TU) (THA) of liquid-propellant rocket engines (LPRE) is given. Principles of the general theory of vane machines are given. The basic calculated relations for the design of the flow part of pumps and turines are derived. The selection of the basic parameters of turbopump units is substantiated, and conditions of their operation are analyzed. Methods of the calculation of pumps and turbines of LPRE are briefly set forth. Examples of the calculation are given.
Book Synopsis Fundamentals of Theory and Calculation of Liquid-propellant Rocket Engines, Volume i by :
Download or read book Fundamentals of Theory and Calculation of Liquid-propellant Rocket Engines, Volume i written by and published by . This book was released on 1969 with total page 300 pages. Available in PDF, EPUB and Kindle. Book excerpt: Theoretical and design principles of liquid rocket engines are presented. Extensive coverage is given to processes taking place in the combustion chamber, calculations of mixing systems, the cooling and contour calculation of the nozzles, calculation and selection of optimal parameters, turbopump and fuel feed pressurization systems, generation of the working medium for the turbine and fuel feed pressurization system, design and integration of pneumohydraulic systems for liquid rocket engines, calculation methods and selection of a liquid rocket engine parameters with a closed generation circuit of the working medium for the turbine. Basic theoretical and design principles of processes taking place in different types of liquid rocket engines are presented. The operation of main subsystems and the calculation of their characteristics are discussed. (Author).
Book Synopsis Fundamentals of Theory and Calculation of Liquid-propellant Rocket Engines by : A. P. Vasilev
Download or read book Fundamentals of Theory and Calculation of Liquid-propellant Rocket Engines written by A. P. Vasilev and published by . This book was released on 1969 with total page 308 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report presents theory and calculations of mechanics involved in operation of a liquid rocket engine.
Book Synopsis Fundamental Concepts of Liquid-Propellant Rocket Engines by : Alessandro de Iaco Veris
Download or read book Fundamental Concepts of Liquid-Propellant Rocket Engines written by Alessandro de Iaco Veris and published by Springer Nature. This book was released on 2020-09-26 with total page 747 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book is intended for students and engineers who design and develop liquid-propellant rocket engines, offering them a guide to the theory and practice alike. It first presents the fundamental concepts (the generation of thrust, the gas flow through the combustion chamber and the nozzle, the liquid propellants used, and the combustion process) and then qualitatively and quantitatively describes the principal components involved (the combustion chamber, nozzle, feed systems, control systems, valves, propellant tanks, and interconnecting elements). The book includes extensive data on existing engines, typical values for design parameters, and worked-out examples of how the concepts discussed can be applied, helping readers integrate them in their own work. Detailed bibliographical references (including books, articles, and items from the “gray literature”) are provided at the end of each chapter, together with information on valuable resources that can be found online. Given its scope, the book will be of particular interest to undergraduate and graduate students of aerospace engineering.
Book Synopsis Fundamentals of Theory and Calculation of Liquid-propellant Rocket Engines by : A. P. Vasilev
Download or read book Fundamentals of Theory and Calculation of Liquid-propellant Rocket Engines written by A. P. Vasilev and published by . This book was released on 1969 with total page 287 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report describes the functioning elements of liquid rocket engines and expounds basic rocket theory.
Book Synopsis Fundamentals of Theory and Calculation of Liquid-propellant Rocket Engines by : A. P. Vasilyev
Download or read book Fundamentals of Theory and Calculation of Liquid-propellant Rocket Engines written by A. P. Vasilyev and published by . This book was released on 1969 with total page 871 pages. Available in PDF, EPUB and Kindle. Book excerpt: Theoretical and design principles of liquid rocket engines are presented. Extensive coverage is given to processes taking place in the combustion chamber, calculations of mixing systems, the cooling and contour calculation of the nozzles, calculation and selection of optimal parameters, turbopump and fuel feed pressurization systems, generation of the working medium for the turbine and fuel feed pressurization system, design and integration of pneumohydraulic systems for liquid rocket engines, calculation methods and selection of a liquid rocket engine parameters with a closed generation circuit of the working medium for the turbine. Basic theoretical and design principles of processes taking place in different types of liquid rocket engines are presented. The operation of main subsystems and the calculation of their characteristics are discussed. (Author).
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 668 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.
Download or read book דיבורי אמונה written by and published by . This book was released on 2002 with total page 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 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 Design of Liquid Propellant Rocket Engines by : Dr Jim Ras
Download or read book Design of Liquid Propellant Rocket Engines written by Dr Jim Ras and published by Lulu.com. This book was released on 2016-09-20 with total page 414 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book intends to build a bridge for the student and the young engineer: to link the rocket propulsion fundamentals and elements (which are well covered in the literature) with the actual rocket engine design and development work as it is carried out in industry (which is very little, if at all covered in literature). The book attempts to further the understanding of the realistic application of liquid rocket propulsion theories, and to help avoid or at least reduce time and money consuming errors and disappointments. In so doing, it also attempts to digest and consolidate numerous closely related subjects, hitherto often treated as separate, bringing them up to date at the same time.
Book Synopsis Design of Liquid Propellant Rocket Engines by : Dieter K. Huzel
Download or read book Design of Liquid Propellant Rocket Engines written by Dieter K. Huzel and published by . This book was released on 1971 with total page 474 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Internal Combustion Processes of Liquid Rocket Engines by : Zhen-Guo Wang
Download or read book Internal Combustion Processes of Liquid Rocket Engines written by Zhen-Guo Wang and published by John Wiley & Sons. This book was released on 2016-08-29 with total page 392 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Theory of Liquid-propellant Rocket Engines by : A. V. Kvasnikov
Download or read book Theory of Liquid-propellant Rocket Engines written by A. V. Kvasnikov and published by . This book was released on 1960 with total page 300 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Liquid Rocket Engines by : Evgeniĭ Borisovich Volkov
Download or read book Liquid Rocket Engines written by Evgeniĭ Borisovich Volkov and published by . This book was released on 19?? with total page 659 pages. Available in PDF, EPUB and Kindle. Book excerpt: In the book the principles of the theory and calculation of units of liquid rocket engines (combustion chambers, pumps, turbines, gas generators). We give the static and dynamic characteristics of the engine. In addition to principles of the theory of individual units we examine the operation of the engine as a whole, i.e., the operation of the engine as an assembly of interconnected units. The basic aim of the book is to acquaint the reader with the theory of the units of modern liquid rocket engines. (Author).
Book Synopsis Liquid Fuel Rocket Engines. Design Fundamentals by : M. V. Dobrovolskii
Download or read book Liquid Fuel Rocket Engines. Design Fundamentals written by M. V. Dobrovolskii and published by . This book was released on 1969 with total page 315 pages. Available in PDF, EPUB and Kindle. Book excerpt: The book presents design fundamentals of liquid fuel rocket engines (ZhRD). It considers questions of design of the engine chamber and the propulsion system on the whole. Basic statements of the theory, methods of calculation and description of subassemblies and units of devices with liquid fuel rocket engine are given. Processes of expansion of gases in nozzles, carburetion and heat exchange are expounded, as well methods of profiling nozzles, calculation of injectors, determination of forms and volumes of combustion chambers. An analysis of work of installations with open and closed circuits is given. Supply systems with turbopump assemblies and pressure feed systems with gas, powder, and liquid pressure generators are considered. Much attention is allotted to work of installations with closed circuits and methods of power coordination of such circuits. Examples of propulsion systems were given, in particular, a description of the propulsion system of the rocket 'Vostok.' (Author).
Book Synopsis Fundamentals of Rocket Propulsion by : DP Mishra
Download or read book Fundamentals of Rocket Propulsion written by DP Mishra and published by CRC Press. This book was released on 2017-07-20 with total page 364 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
