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Author : Dieter K. Huzel
Publisher : AIAA
Page : 452 pages
File Size : 53,6 Mb
Release : 1992
Category : Liquid propellant rocket engines
ISBN : 1600864007
Author : George Paul Sutton
Publisher : AIAA
Page : 936 pages
File Size : 49,6 Mb
Release : 2006
Category : Technology & Engineering
ISBN : 1563476495
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 : Alessandro de Iaco Veris
Publisher : Springer Nature
Page : 747 pages
File Size : 41,9 Mb
Release : 2020-09-26
Category : Technology & Engineering
ISBN : 9783030547042
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.
Author : Vigor Young
Publisher : AIAA
Page : 606 pages
File Size : 55,9 Mb
Release : 1995
Category : Liquid propellant rockets
ISBN : 160086418X
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.
Author : David Altman
Publisher : Princeton University Press
Page : 197 pages
File Size : 55,5 Mb
Release : 2015-12-08
Category : Science
ISBN : 9781400879953
David Altman, James M. Carter, S. S. Penner, Martin Summerfield. High Temperature Equilibrium, Expansion Processes, Combustion of Liquid Propellants, The Liquid Propellants Rocket Engine. Originally published in 1960. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Author : L.E. Bollinger
Publisher : Elsevier
Page : 699 pages
File Size : 46,7 Mb
Release : 2013-04-22
Category : Science
ISBN : 9780323163330
Liquid Rocket and Propellants
Author : Mark L. Dranovsky
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 352 pages
File Size : 46,6 Mb
Release : 2007
Category : Technology & Engineering
ISBN : 1563479214
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 : David T. Harrje,Frederick H. Reardon
Publisher : Unknown
Page : 674 pages
File Size : 42,7 Mb
Release : 1972
Category : Liquid propellant rockets
ISBN : UIUC:30112007520619
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.
Author : Leon M. Wenzel
Publisher : Unknown
Page : 18 pages
File Size : 49,6 Mb
Release : 1965
Category : Liquid oxygen
ISBN : UIUC:30112106635771
Author : Rene Nardi Rezende
Publisher : SAE International
Page : 158 pages
File Size : 43,6 Mb
Release : 2018-11-15
Category : Technology & Engineering
ISBN : 9780768095425
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.
Author : Vigor Yang
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 776 pages
File Size : 42,5 Mb
Release : 2004
Category : Science
ISBN : UOM:39015059149578
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.
Author : Zhen-Guo Wang
Publisher : John Wiley & Sons
Page : 392 pages
File Size : 47,5 Mb
Release : 2016-08-29
Category : Technology & Engineering
ISBN : 9781118890028
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 : H. J. Ellis
Publisher : Unknown
Page : 156 pages
File Size : 54,5 Mb
Release : 1973
Category : Liquid propellant rockets
ISBN : NASA:31769000661606
Author : John R. Szuch
Publisher : Unknown
Page : 44 pages
File Size : 45,8 Mb
Release : 1969
Category : Combustion
ISBN : UIUC:30112106876425
Double-dead-time model describing chugging to liquid propellant rocket engines having multielement injectors.
Author : Stephen D. Heister,William E. Anderson,Timothée L. Pourpoint,R. Joseph Cassady
Publisher : Cambridge University Press
Page : 589 pages
File Size : 49,8 Mb
Release : 2019-02-07
Category : Science
ISBN : 9781108422277
Equips students with an up-to-date practical knowledge of rocket propulsion, numerous homework problems, and online self-study materials.
