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Author : F. Lillo
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Burning Rate Mechanisms of Solid Propellants written by F. Lillo and published by . This book was released on 2003 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Vigor Yang
Publisher : AIAA
ISBN 13 : 9781600864377
Total Pages : 1038 pages
Book Rating : 4.8/5 (643 download)
Download or read book Solid Propellant Chemistry Combustion and Motor Interior Ballistics 1999 written by Vigor Yang and published by AIAA. This book was released on 2000 with total page 1038 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Martin Summerfield
Publisher : AIAA
ISBN 13 : 9781600863967
Total Pages : 922 pages
Book Rating : 4.8/5 (639 download)
Download or read book Nonsteady Burning and Combustion Stability of Solid Propellants written by Martin Summerfield and published by AIAA. This book was released on 1992 with total page 922 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : S. R. Chakravarthy
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Mechanism of Burning Rate Enhancement of Composite Solid Propellants by Ferric Oxide written by S. R. Chakravarthy and published by . This book was released on 1995 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : A. C. Eringen
Publisher : Elsevier
ISBN 13 : 148322340X
Total Pages : 648 pages
Book Rating : 4.4/5 (832 download)
Download or read book Mechanics and Chemistry of Solid Propellants written by A. C. Eringen and published by Elsevier. This book was released on 2014-06-28 with total page 648 pages. Available in PDF, EPUB and Kindle. Book excerpt: Mechanics and Chemistry of Solid Propellants is a collection of papers presented at the Fourth Symposium on Naval Structural Mechanics, held in Purdue University, Lafayette, Indiana on April 19-21, 1965 under the joint sponsorship of the Office of Naval Research and Purdue University. The contributors consider the development and utilization of solid propellants. This book is composed of 22 chapters that cover the many branches of studies that touch upon the science and technology of solid propellants. Some chapters present the mathematical and physical theories underlying the behavior of solid propellants, such as nonlinear and linear theories of viscoelasticity. Other chapters are devoted to advances in solid propellant binder chemistry; combustion and its effects on the structural integrity of the solid propellant grain; and design and other engineering problems. This book will be of value to scientists, engineers, and researchers who are interested in the diverse applications of solid propellants.
Author : Martin Summerfield
Publisher : Elsevier
ISBN 13 : 0323163351
Total Pages : 713 pages
Book Rating : 4.3/5 (231 download)
Download or read book Solid Propellant Rocket Research written by Martin Summerfield and published by Elsevier. This book was released on 2013-11-11 with total page 713 pages. Available in PDF, EPUB and Kindle. Book excerpt: Solid Propellant Rocket Research
Author : David A. Flanigan
Publisher :
ISBN 13 :
Total Pages : 31 pages
Book Rating : 4.:/5 (227 download)
Download or read book Combustion Mechanism of High Burning Rate Solid Propellants written by David A. Flanigan and published by . This book was released on 1967 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt: Thiokol's program to tailor the burning rate of a propellant predictably and controllably to any desired level in the range from one to ten inches per second is divided into three phases: Phase I-Synthesis of Burning Rate Catalysts, Phase II-Decomposition Studies and Evaluation of Catalysts and Phase III-Decomposition of Advanced Oxidizers, Fuels, and Binders. Experiments will be performed to synthesize more efficient burn rate catalysts by maximizing already determined guideline properties toward development of an ideal catalyst under Phases I and II. Following catalyst synthesis, each compound showing potential will be subjected to comprehensive decomposition studies and combustion mechanism evaluation with propellant ingredients. To date, 30 candidate catalysts materials have been synthesized and the physical properties ascertained. Compatibility testing of these materials is essentially complete and no serious problems are expected in the formulation and scale-up of propellants containing the candidate catalysts. Burn rate studies thus far indicate that several prospective liquid ferrocene derivatives offer considerable potential in increasing burn rates over that presently available with n-butyl ferrocene (PLASTISCAT-IV(R)). (Author).
Author : T.L. Varghese
Publisher : Allied Publishers
ISBN 13 : 9385926330
Total Pages : 326 pages
Book Rating : 4.3/5 (859 download)
Download or read book The Chemistry and Technology of Solid Rocket Propellants (A Treatise on Solid Propellants) written by T.L. Varghese and published by Allied Publishers. This book was released on 2017-03-29 with total page 326 pages. Available in PDF, EPUB and Kindle. Book excerpt: The book is a treatise on solid propellants in nine chapters, covering the history, chemistry, energetics, processing and characterization aspects of composite solid propellants, internal ballistics, advanced solid propellants, safety, quality and reliability and homogenous or double base propellants. The book also traces the evolution of solid propellant technology in ISRO for launch vehicles and sounding rockets. There is a detailed table of contents, expanded index, glossary, exhaustive references and questions in each chapter. It can be used as a textbook for science and engineering students, as a reference book for researchers and as a companion to scientists and engineers working in the research, development and production areas of solid propellants.
Author : Naminosuke Kubota
Publisher : John Wiley & Sons
ISBN 13 : 3527693513
Total Pages : 560 pages
Book Rating : 4.5/5 (276 download)
Download or read book Propellants and Explosives written by Naminosuke Kubota and published by John Wiley & Sons. This book was released on 2015-04-23 with total page 560 pages. Available in PDF, EPUB and Kindle. Book excerpt: This third edition of the classic on the thermochemical aspects of the combustion of propellants and explosives is completely revised and updated and now includes a section on green propellants and offers an up-to-date view of the thermochemical aspects of combustion and corresponding applications. Clearly structured, the first half of the book presents an introduction to pyrodynamics, describing fundamental aspects of the combustion of energetic materials, while the second part highlights applications of energetic materials, such as propellants, explosives and pyrolants, with a focus on the phenomena occurring in rocket motors. Finally, an appendix gives a brief overview of the fundamentals of aerodynamics and heat transfer, which is a prerequisite for the study of pyrodynamics. A detailed reference for readers interested in rocketry or explosives technology.
Author : Alexander S. Shteinberg
Publisher : Springer Science & Business Media
ISBN 13 : 3540788611
Total Pages : 203 pages
Book Rating : 4.5/5 (47 download)
Download or read book Fast Reactions in Energetic Materials written by Alexander S. Shteinberg and published by Springer Science & Business Media. This book was released on 2008-09-26 with total page 203 pages. Available in PDF, EPUB and Kindle. Book excerpt: Modern energetic materials include explosives, blasting powders, pyrotechnic m- tures and rocket propellants [1, 2]. The study of high-temperature decomposition of condensed phases of propellants and their components (liquid, solid and hybrid) is currently of special importance for the development of space-system engineering [3, 4]. To better understand the burning mechanisms (stationary, nonstationary, - steady) of composite solid propellants and their components, information about the macrokinetics of their high-temperature decomposition is required [5]. To be able to evaluate the ignition parameters and conditions of safe handling of heat-affected explosives, one needs to know the kinetic constants of their high-temperature - composition. The development of new composite solid propellants characterized by high performance characteristics (high burning rates, high thermal stability, stability to intrachamber perturbations, and other aspects) is not possible without quanti- tive data on the high-temperature decomposition of composite solid propellants and their components [6]. The same reasons have resulted in signi?cant theoretical and practical interest in the high-temperature decomposition of components of hybrid propellants. It is known that hybrid propellants have not been used very widely due to the low bu- ing (pyrolysis) rates of the polymer blocks in the combustion chambers of hybrid rocket engines. To increase the burning rates it is necessary to obtain information about their relationships to the corresponding kinetic and thermophysical prop- ties of the fuels.
Author : Clayton Huggett
Publisher : Princeton University Press
ISBN 13 : 1400879078
Total Pages : 175 pages
Book Rating : 4.4/5 (8 download)
Download or read book Solid Propellant Rockets written by Clayton Huggett and published by Princeton University Press. This book was released on 2015-12-08 with total page 175 pages. Available in PDF, EPUB and Kindle. Book excerpt: Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material or to eliminate cross reference to other portions of the original volumes. 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.
Author : Martin S. Miller
Publisher :
ISBN 13 : 9781423548195
Total Pages : 68 pages
Book Rating : 4.5/5 (481 download)
Download or read book CYCLOPS, A Breakthrough Code to Predict Solid-Propellant Burning Rates written by Martin S. Miller and published by . This book was released on 2003-02 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: Theoretical capability to predict the burning rate of real propellants from their ingredients would be an invaluable aid to formulating new propellants. Despite progress over the last decade on a very few simple ingredients, such as cyclotrimethylenetrintramine (RDX), and a few simple binary mixtures, no general capability of this sort exists today. This shortcoming is not due to insufficient computational resources, but to a lack of understanding of fundamental combustion mechanisms in the condensed phase and surface(gas interlace for typical propellant ingredients and their mixtures. This difficult problem is likely to remain intractable for some time to come. In this report, we demonstrate that our previously published semi-empirical formalism for single ingredients can be success fully extended to treat multi-ingredient propellants. In particular, for purposes of this report, we confine ourselves to nitrate- ester propellants, using MlO, M2, M9, and JA2 as examples. However, the method should also be applicable to other classes of homogeneous propellants and even composite propellants where mixing of ingredients in a surface melt layer or sufficiently small particle sizes remove the multi- dimensional character. The method treats the gas-phase processes on the level of elementary reaction and multicomponent transport. A semi-empirical pyrolysis law coupled with informed estimates of the decomposition products of the condensed phase enables us to finesse the absence of knowledge of the detailed processes occurring in the condensed phase and at the burning surface. Results of a computer code, CYCLOPS, based on this approach, show that both the burning rate and flame structure are well predicted for a series of four U. S. Army gun propellants.
Author :
Publisher :
ISBN 13 :
Total Pages : 656 pages
Book Rating : 4.:/5 (318 download)
Download or read book Mechanics and Chemistry of Solid Propellants written by and published by . This book was released on 1967 with total page 656 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Lewis J. Hurt
Publisher :
ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)
Download or read book The Study of the Mechanism of Enhanced Burning Rate of Solid Propellants written by Lewis J. Hurt and published by . This book was released on 1964 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: In this paper, the problem of burning-rate en hancement of solid propellants by incorporating metallic wires into the propellant matrix is treated by utilizing heat-transfer theory and geometry. It was found that heat conduction considerations incorporating the moving-heat-source restriction to the Fourier equation would adequately describe the process of 'coning' and that the geometrical considerations of the coned surface together with the P-K-r data for the matrix propellant would give excellent predictions of the burning rate enhancement. The effects of wire length, wire concentration, and increased burning-rate pressure exponents due to the addition of wire are discussed. Experimental and theoretical P-r plots are presented for a typical staple-containing composite double-base propellant. (Author).
Author :
Publisher :
ISBN 13 :
Total Pages : 108 pages
Book Rating : 4.:/5 (227 download)
Download or read book INVESTIGATION OF THE MECHANISM OF SOLID PROPELLANT BURN RATE. written by and published by . This book was released on 1967 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: The mechanism by which iron compounds catalyze the burning rate of solid composite propellants is reported. A series of experiments were conducted to define the efficacy of iron compounds on burning rate. Experiments performed under Phases I and II studies, which were designed to study the interaction, if any, between catalysts and oxidizer and binder indicate the following conclusions. Thermal decomposition of ammonium perchlorate under pressure occurs in a single-phase step instead of the three phases observed at atmospheric pressure. The singe-phase decomposition step of ammonium perchlorate is shifted to lower temperature in the presence of iron oxide. The degree of this shift is dependent upon Fe2O3 concentration. The autoignition temperature of composite propellant decreases with increasing pressure. The rate of decomposition of anhydrous perchloric acid on varied surfaces seems to be a strong function of exposed specific surface of the catalyst and not overly dependent upon the chemical nature of the material. Iron compounds such as Fe2O3, ferrocene and butyl ferrocene do not facilitate the pyrolysis of polybutadiene polymers or gumstocks. A mechanism for catalysis by iron compounds is presented and mathematical expressions relating the variables involved have been formulated.
Author : K. K. Kuo
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (847 download)
Download or read book Fundamentals of Solid Propellant Combustion written by K. K. Kuo and published by . This book was released on 1995 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Vigor Yang
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
ISBN 13 :
Total Pages : 1044 pages
Book Rating : 4.3/5 (91 download)
Download or read book Solid Propellant Chemistry, Combustion, and Motor Interior Ballistics written by Vigor Yang and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 2000 with total page 1044 pages. Available in PDF, EPUB and Kindle. Book excerpt: This volume brings together the world's most highly regarded scientists in the field of solid rocket propulsion. Thirty-nine papers present in-depth coverage on a wide range of topics including: advanced materials and nontraditional formulations; the chemical aspects of organic and inorganic components in relation to decomposition mechanisms, kinetics, combustion, and modeling; safety issues, hazards and explosive characteristics; and experimental and computational interior ballistics research, including chemical information and the physics of the complex flowfield.
