THEORY OF COMBUSTION INSTABILITY IN LIQUID PROPELLANT ROCKET MO
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DOWNLOAD EBOOKAuthor: David T. Harrje
Publisher:
Published: 1972
Total Pages: 668
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DOWNLOAD EBOOKThe 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: Luigi CROCCO (and CHENG (Sin-I))
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Published: 1956
Total Pages: 0
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DOWNLOAD EBOOKAuthor: Luigi Crocco
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Published: 1956
Total Pages: 216
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DOWNLOAD EBOOKThe report presents a theoretical analysis of combustion instability in liquid rocket motors.
Author: Vigor Young
Publisher: AIAA
Published: 1995
Total Pages: 606
ISBN-13: 9781600864186
DOWNLOAD EBOOKAnnotation 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.
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Published: 1972
Total Pages: 668
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DOWNLOAD EBOOKAuthor: Ben T. Zinn
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Published: 1966
Total Pages:
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DOWNLOAD EBOOKAuthor: David T. Harrje
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Published: 1972
Total Pages: 0
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DOWNLOAD EBOOKAuthor: Mark L. Dranovsky
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
Published: 2007
Total Pages: 352
ISBN-13: 9781563479212
DOWNLOAD EBOOKThis 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: Manuel Edward Lores
Publisher:
Published: 1972
Total Pages: 396
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