Liquid Rocket Engine Combustion Instability
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| Author | : Mark L. Dranovsky |
| Publisher | : AIAA (American Institute of Aeronautics & Astronautics) |
| Total Pages | : 352 |
| Release | : 2007 |
| Genre | : Technology & Engineering |
| ISBN | : 9781563479212 |
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 | : Vigor Young |
| Publisher | : AIAA |
| Total Pages | : 606 |
| Release | : 1995 |
| Genre | : Liquid propellant rockets |
| ISBN | : 9781600864186 |
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 | : Miron Semenovich Natanzon |
| Publisher | : AIAA (American Institute of Aeronautics & Astronautics) |
| Total Pages | : 298 |
| Release | : 1999 |
| Genre | : Science |
| ISBN | : |
First published in 1986 by Mashinostroenie, Moscow.
| Author | : L.E. Bollinger |
| Publisher | : Elsevier |
| Total Pages | : 699 |
| Release | : 2013-04-22 |
| Genre | : Science |
| ISBN | : 0323163335 |
Liquid Rocket and Propellants
| Author | : Dieter K. Huzel |
| Publisher | : AIAA |
| Total Pages | : 452 |
| Release | : 1992 |
| Genre | : Liquid propellant rocket engines |
| ISBN | : 9781600864001 |
| Author | : Stephen D. Heister |
| Publisher | : Cambridge University Press |
| Total Pages | : 589 |
| Release | : 2019-02-07 |
| Genre | : Science |
| ISBN | : 1108422276 |
Equips students with an up-to-date practical knowledge of rocket propulsion, numerous homework problems, and online self-study materials.
| Author | : |
| Publisher | : |
| Total Pages | : 648 |
| Release | : 1963 |
| Genre | : Aeronautics |
| ISBN | : 9781563477034 |
| Author | : David T. Harrje |
| Publisher | : |
| Total Pages | : 668 |
| Release | : 1972 |
| Genre | : Liquid propellant rockets |
| ISBN | : |
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 | : DP Mishra |
| Publisher | : CRC Press |
| Total Pages | : 364 |
| Release | : 2017-07-20 |
| Genre | : Technology & Engineering |
| ISBN | : 1351708414 |
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 | : A. Davenas |
| Publisher | : Newnes |
| Total Pages | : 623 |
| Release | : 2012-12-02 |
| Genre | : Technology & Engineering |
| ISBN | : 0080984754 |
This book, a translation of the French title Technologie des Propergols Solides, offers otherwise unavailable information on the subject of solid propellants and their use in rocket propulsion. The fundamentals of rocket propulsion are developed in chapter one and detailed descriptions of concepts are covered in the following chapters. Specific design methods and the theoretical physics underlying them are presented, and finally the industrial production of the propellant itself is explained. The material used in the book has been collected from different countries, as the development of this field has occurred separately due to the classified nature of the subject. Thus the reader not only has an overall picture of solid rocket propulsion technology but a comprehensive view of its different developmental permutations worldwide.
