
Combustion Instabilities in Liquid Rocket Engines
Testing and Development Practices in Russia
American Institute of Aeronautics & Astronautics (Publisher)
Published on 1. October 2007
Book
Hardback
285 pages
978-1-56347-921-2 (ISBN)
Description
This is the first book to cover development and testing practices for liquid rocket engines in Russia and the former Soviet Union.
More details
Product info
Hardback
Series
Language
English
Place of publication
Reston
United States
Target group
Professional and scholarly
Product notice
sewn/stitched
Paper over boards
Illustrations
Illustrations
Dimensions
Height: 234 mm
Width: 157 mm
Thickness: 23 mm
Weight
590 gr
ISBN-13
978-1-56347-921-2 (9781563479212)
Copyright in bibliographic data and cover images is held by Nielsen Book Services Limited or by the publishers or by their respective licensors: all rights reserved.
Schweitzer Classification
Persons
Mark Dranovsky, Doctor of Technical Sciences, was the head of the Scientific Department of the Research Institute of Chemical Engineering, NIICHIMMASH, the leading institution in the former Soviet Union and Russia in the evaluation and research of liquid rocket combustion instability. Dr. Dranovsky took part in the development of numerous rocket engines with General Designers S.P. Korolev, V.P. Glushko, M.K. Yangel, V.P. Makeev, V.P. Radovsky, A.D. Konopatov, and M.K. Kuznetsov. Vigor Yang is John L. and Genevieve H. McCain Chair in Engineering at the Pennsylvania State University. He also serves as the Editor-in-Chief of the Journal of Propulsion and Power and is the author/editor of several books on rocket and air-breathing propulsion. Fred Culick is Richard L. and Dorothy M. Hayman Professor of Mechanical Engineering (Retired) at the California Institute of Technology. He is the editor of the book by M.S. Natanzon, Combustion Instability, to be published by the AIAA, which treats Russian theoretical work concerned with the same problems addressed experimentally by the methods discussed in the present volume. Doug Talley is senior research scientist in the Aerophysics Branch of the Air Force Research Laboratory, where he has conducted research in liquid propellant rocket combustion for the past 16 years. He is an associate editor of the Journal of Propulsion and Power and author of numerous articles and papers on liquid propellant rocket injectors and combustion.
Content
Introduction; Terms and Definitions; Mechanisms of Transition from Noise to High-Frequency Oscillations or to Noise at a New Level.