5 edition of Solid Propellant Chemistry Combustion and Motor Interior Ballistics 1999 (Progress in Astronautics and Aeronautics) found in the catalog.
by AIAA (American Institute of Aeronautics & Ast
Written in English
|Contributions||Vigor Yang (Editor)|
|The Physical Object|
|Number of Pages||990|
Burning Rate Augmentation of BAMO Based Propellants. Yoshio Oyumi. Third Research Center, Technical Research and Development Institute, Japan Defense Agency, 1–2–10 Sakae, Tachikawa, Tokyo (Japan) Solid Propellant Chemistry, Combustion, and Motor Interior Ballistics, /, (), (). Crossref. 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.
Solid rocket motor internal ballistics simulation using different burning rate models 51 For many double-base propellants, also referred to as smokeless powders, it was established that the burning rates obey a relationship known as Vieille’s or Saint Robert’s empirical . Combustion of Solid Propellants The combustion of the components and then of the various propellants will be seen in the next chapters. A few general references about chemical propulsion, solid propellants and combustion can be found at the end of the main text, ahead of more specialized references introduced progressively in the followingCited by:
Astronautics, Rocketry, Spacecraft, and Space Technology Recommended books, monographs, textbooks, college textbooks, tutorials E. Mallove and G. Matloff, The Starflight Handbook. A Pioneer's Guide to Interstellar Travel, Wiley, Solid Propellant Chemistry Combustion and Motor Interior Ballistics, AIAA, C.D. Brown. A general numerical model based on the Zeldovich-Novozhilov solid-phase energy conservation result for unsteady solid-propellant burning is presented in this paper. Unlike past models, the integrated temperature distribution in the solid phase is utilized directly for estimating instantaneous burning rate (rather than the thermal gradient at the burning surface).Cited by:
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Solid Propellant Chemistry Combustion and Motor Interior Ballistics (Progress in Astronautics & Aeronautics) by Professor Vigor Yang (Editor), Thomas B Brill (Editor), Wu-Zhen Ren (Editor), Paul Zarchan (Editor) & 1 more4/5(2). Solid Propellant Chemistry Combustion and Motor Interior Ballistics Vigor Yang.
AIAA, - Ballistics, Interior - pages. 1 Review. Preview this book» What people are saying - Write a review. User Review - Flag as inappropriate. This book is full of information.
I cant buy as it has very high price.I want to get it free online 5/5(1). Solid Propellant Chemistry, Combustion, and Motor Interior Ballistics. and experimental and computational interior ballistics research, including chemical information and the physics of the complex flowfield.
Combustion Dynamics of Homogenous Solid Propellants in a Rocket Motor with Acoustic Excitations. – Description: 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. Have spare times. Read Solid Propellant Chemistry Combustion and Motor Interior Ballistics (Progress in Astronautics &.
Need a fantastic electronic book. Solid Propellant Chemistry Combustion and Motor Interior Ballistics (Progress in Astronautics & by Author, the very best one. Wan na get it. Abstract: Description. 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.
Solid propellant chemistry, combustion, and motor interior ballistics. Reston, Va.: American Institute of Aeronautics and Astronautics, © (OCoLC) Document Type: Book: All Authors / Contributors: Vigor Yang; Thomas B Brill; Wu-Zhen Ren.
Fire resulted lb burning solid-propellant burning at °F. Heat, acid vapors, and smoke filled surrounding area impeding escaping personnel from compartments. Second missile hit, penetrated hull, and detonated 5-ft inboard.
Detonation ripped large hole in hull, accelerating combustion of burning materials. Solid propellant chemistry, combustion, and motor interior ballistics. Reston, Va.: American Institute of Aeronautics and Astronautics, © (DLC) (OCoLC) Material Type: Document, Internet resource: Document Type: Internet Resource, Computer File: All Authors / Contributors: Vigor Yang; Thomas B Brill; Wu-Zhen Ren.
Solid Propellant Chemistry, Combustion, and Motor Interior Ballistics 作者: Ren, Wu-Zhen 编 页数: 定价: $ ISBN: 豆瓣评分. Solid Propellant Chemistry, Combustion, and Motor Interior Ballistics - Progress in Astronautics and Aeronautics, Volume Details This book brings together the world’s most highly regarded scientists in the field of solid rocket propulsion and provides in.
Addressing both experimental as well as theoretical aspects, the book covers the thermochemical and combustion characteristics of all important types of energetic materials, such as explosives, propellants, and the new class of pyrolants, as well as related phenomena.
Solid Propellant Chemistry Combustion and Motor Interior Ballistics (Progress in Astronautics & Aeronautics) by Yang, Professor Vigor Format: Hardcover Change4/5. and computational interior ballistics research, overviewed in Part III, is moving quickly to include chemical information and the physics of the complex flow field.
One motivation for melding the areas of chemistry and turbulent flows is the hope of eventually learning how to control combustion dynamics in solid rocket motors. Abstract. The paper deals with mathematical simulation of dispersion of agglomerates formed in combustion of aluminized solid propellants.
A substantial effect of the separation conditions of agglomerating metal particles from the surface of the burning propellant on the size of Cited by: This chapter discusses the solid propellant combustion and internal ballistics of motors. The combustion of a solid propellant is characterized by the way its surface regresses once it begins to burn.
The burning rate is the distance traveled by the flame front per unit of time, measured normally to the burning by: The book also goes on to discuss the combustion mechanisms of various types of energetic materials, propellants, and explosives, based on the heat transfer process in the combustion waves.
The combustion efficiency of metallized propellants are investigated and compared to the corresponding blank propellant in order to evaluate the actual effect of the metals in solid rocket. Solid propellant chemistry condensed phase behaviour of ammonium perchlorate-based solid propellants by K.
Kishore. Published by Defence Research & Development Organisation, Ministry of Defence in New Delhi. Written in EnglishPages: The properties of the surface layer of burning metallized solid propellants are analyzed on the basis of available experimental data.
A general physical concept of processes in the surface layer is developed. The structure called a skeleton layer is shown to play a key role in combustion. The factors influencing the properties of the skeleton layer are determined, and the effect of these of Cited by:. The full text of this article hosted at is unavailable due to technical difficulties.Studies on solid propellant combustion modeling have been an integral part of understanding the characteristics of the burning rates and flame structure, such as temperature and species profiles.
Current models, e.g. the two-phase approach embodied in the CYCLOPS code, are useful for both single- and multi-ingredient mixtures , .Cited by: 3.Review of Solid Propellant Ignition Models Relative to the Interior Ballistic Modelling of Gun Systems Executive Summary Solid propellant ignition (and the evolution to self-sustained combustion) is a highly complex physicochemical process, involving the transition of a stable solid propellant stateCited by: 2.