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Book
Theory of combustion instability in liquid propellant rocket motors
Authors: ---
Year: 1956 Volume: no. 8 Publisher: [London] : Published for and on behalf of the Advisory Groupfor Aeronautical Research and Development, North Atlantic Treaty Organization by Butterworths Scientific Publications,

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Book
Precision flow measurement techniques for low-thrust auxiliary propulsion liquid rockets
Authors: ---
Year: 1967 Publisher: [Washington, D.C.] : [National Aeronautics and Space Administration],

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Modern engineering for design of liquid-propellant rocket engines
Authors: --- ---
ISBN: 9781563470134 1563470136 Year: 1992 Publisher: Washington, DC : American Institute of Aeronautics and Astronautics,

History of liquid propellant rocket engines
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ISBN: 1563476495 Year: 2006 Publisher: Reston, VA : American Institute of Aeronautics and Astronautics,

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Book
Digital computer program for analysis of chugging instabilities
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Year: 1970 Publisher: Washington, D.C. : National Aeronautics and Space Administration,

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Book
Liquid rocket booster study. : final report.
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Year: 1989 Publisher: San Diego, California : General Dynamics, Space Systems Division,

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Book
Liquid propellant rockets
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ISBN: 1400879957 0691652333 Year: 1960 Publisher: Princeton, New Jersey : Princeton University Press,

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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.


Book
America's first rocket company : Reaction Motors, Inc.
Authors: ---
ISBN: 1624104428 Year: 2017 Publisher: Reston, VA : American Institute of Aeronautics and Astronautics, Inc.,

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The rocket and the Reich : Peenemünde and the coming of the ballistic missile era
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ISBN: 0029228956 Year: 1995 Publisher: New York ; London ; Singapore The Free Press

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Book
Fundamental concepts of liquid-propellant rocket engines
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ISBN: 3030547043 3030547035 Year: 2021 Publisher: Cham, Switzerland : Springer,

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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.

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