An Investigation of Instabilities Characteristic of Liquid Propellant Rocket Motors
Author :
Publisher :
Page : 80 pages
File Size : 15,20 MB
Release : 1952
Category : Liquid propellant rockets
ISBN :
Author :
Publisher :
Page : 80 pages
File Size : 15,20 MB
Release : 1952
Category : Liquid propellant rockets
ISBN :
Author : Vigor Young
Publisher : AIAA
Page : 606 pages
File Size : 29,23 MB
Release : 1995
Category : 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 : David T. Harrje
Publisher :
Page : 674 pages
File Size : 18,50 MB
Release : 1972
Category : 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 :
Publisher :
Page : 0 pages
File Size : 14,84 MB
Release : 1999
Category :
ISBN :
This study investigated the feasibility of active control of combustion instabilities in liquid fueled combustors using a liquid fuel injector actuator and adaptive control of combustion instabilities. Two different liquid fuel injector actuators were developed and their performance was investigated in open and closed loop active control tests. The open loop tests have shown that these actuators can effectively produce coherent, large amplitude, heat release oscillations with nearly constant phase over a wide range of frequencies, thus indicating that they could be employed to damp combustion instabilities. Furthermore, cold and reactive flow tests have shown that the performance of the liquid fuel actuators depends upon the injector's design and the characteristics of its spray. In parallel efforts, an adaptive control approach that does not require apriori knowledge of the open loop response of the control system is being investigated. The system "forces" the unstable combustor with a controlled, slowly varying, disturbance and uses the measured response of the combustor to determine the optimum control system phase and gain. Initial results obtained with this system are promising. This study also investigated the use of piezoelectric actuators to drive the fuel injector actuators in an effort to reduce their size and weight.
Author : Mark L. Dranovsky
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 352 pages
File Size : 28,17 MB
Release : 2007
Category : 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 : Frederick Henry Reardon
Publisher :
Page : pages
File Size : 14,1 MB
Release : 1961
Category : Combustion
ISBN :
Author : Luigi Crocco
Publisher :
Page : 216 pages
File Size : 19,30 MB
Release : 1956
Category : Combustion
ISBN :
The report presents a theoretical analysis of combustion instability in liquid rocket motors.
Author : David T. Harrje
Publisher :
Page : 668 pages
File Size : 39,96 MB
Release : 1972
Category : 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 : L.E. Bollinger
Publisher : Elsevier
Page : 699 pages
File Size : 20,84 MB
Release : 2013-04-22
Category : Science
ISBN : 0323163335
Liquid Rocket and Propellants
Author : DP Mishra
Publisher : CRC Press
Page : 364 pages
File Size : 39,36 MB
Release : 2017-07-20
Category : 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.