1 edition of Combustion of solid propellants. found in the catalog.
Combustion of solid propellants.
Sponsored by the Propulsionand Energetics Panel and the Consultant and Exchange Programme of AGARD.
|Series||Agard lecture series -- 180|
|Contributions||Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel., Advisory Group for Aerospace Research and Development. Consultantand Exchange Programme.|
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). This book identifies technological gaps in different areas of solid-propellant combustion and encourages further advancements in solid-propellant propulsion systems so that future systems can be designed and developed with higher efficiency, greater reproducibility, and maximum safety considerations.
It presents the fundamental bases of the energetics of materials, deflagration and detonation, thermochemical process of decomposition and combustion, plus combustion wave structures. The book also goes on to discuss the combustion mechanisms of various types of energetic materials, propellants, and explosives, based on the heat transfer. Solid and liquid propellants are substances that undergo rapid combustion, producing gaseous products. Black powder was used as a propellant in guns and rockets until the 20th century, when double-base gunpowder (40 percent nitroglycerin, 60 percent nitrocellulose) came into use. Other modern solid propellants are Read More; rocket.
A dependence of the burning rate of solid energetic materials on the burning surface curvature is investigated. The model predicts an existence of a limiting value of curvature above which self-sustained combustion is impossible. This result is used for explaining the critical conditions of combustion of homogeneous condensed energetic by: 4. Providing several approaches to stability, safety, and controlled combustion of flammable substances, Thermal Decomposition and Combustion of Explosives and Propellants is a multi-dimensional resource for graduate students, researchers and professionals interested in chemical kinetics, the combustion and synthesis of high-energy materials.
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American Institute of Aeronautics and Astronautics Combustion of solid propellants. book Valley Drive, Suite Reston, VA This book, a translation of the French title Technologie des Propergols Solides, offers otherwise unavailable information on the subject of solid propellants and their use in rocket propulsion.
The fundamentals of rocket propulsion are developed in chapter one and detailed descriptions of concepts are covered in the following chapters. Also reported are detailed analyses of intrinsic combustion stability of solid propellants and stability of solid rocket motors or burners.
The book combines state-of-the-art knowledge with a tutorial presentation of the topics, so that it can be used as a textbook for students or reference for engineers and scientists involved in solid. Solid Propellant Chemistry Combustion and Motor Interior Ballistics (Progress in Astronautics & Aeronautics) [Yang, Professor Vigor, Brill, Thomas B, Ren, Wu-Zhen, Zarchan, Paul] on *FREE* shipping on qualifying offers.
Solid Propellant Chemistry Combustion and Motor Interior Ballistics (Progress in Astronautics & Aeronautics)4/5(2). Book Description. Boron-Based Fuel-Rich Solid Rocket Propellant Technology is a professional book that systematically introduces the latest research progress for boron-based fuel-rich solid covers surface modifications, coating and agglomerating techniques, granulation, and characterization of amorphous boron powders, and its application to fuel-rich solid rocket.
In solid propellants, aluminum plays a key role in energy performance enhancement, but it also induces combustion problems such as low combustion efficiency and agglomeration.
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 burning rate models are also presented as an aid to understanding the rate-controlling steps of combustion processes, thus demonstrating the.
Solid-Phase Region B. Subsurface Multi-Phase Region C. Gas-Phase Region D. Boundary Conditions V. NUMERICAL METHOD VI. DISCUSSION OF MODEL RESULTS A. Steady-State Combustion of Nitramine Propellants B. Laser-Induced Ignition of RDX Monopropellant C.
Steady-State Combustion of HMX/GAP and RDX/GAP Pseudo-Propellants 1. HMX/GAP Pseudo. combustion of most propellants cannot be quenched once it has begun. This chapter primarily considers the risks of expo-sure via inhalation, the skin, and the eyes to the major combustion products of commonly used solid propel-lants—carbon monoxide, ammonia, hydrogen chlo-ride, oxides of nitrogen and sulfur, and lead—in army weapons Size: KB.
The combustion—or, more precisely, the oxidation—of CO and aromatic compounds has been discussed in the book. This information and that to be developed will be used to examine the emission of other combustion-generated compounds thought to have detrimental effects on the environment and on human health.
Description: The Chemistry of Propellants is a collection of papers and comments presented at the meeting on “The Chemistry of Propellants, held in Paris, France on June, organized by the AGARD Combustion and Propulsion Panel. This book is organized into six parts encompassing 25 chapters that serve as an introduction to the.
CHAPTER 14 SOLID PROPELLANT COMBUSTION AND ITS STABILITY. In this the third of four chapters on solid propellant rocket motors we discuss combustion of solid propellants, physical and chemical processes of burning, ignition or start‐up process, extinction of burning, and combustion instability.
adjacent to burning solid propellants. Such techniques provide solid-propellant combustion scientists with the means for measurement of velocities, species concentrations, temperatures, and densities with high spatial and time resolutions.
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 burning rate models are also presented as an aid to understanding the rate-controlling steps of combustion processes, thus demonstrating the Cited by: Solid propellant combustion mechanisms and flame structure Article (PDF Available) in Pure and Applied Chemistry 65(2) February with 1, Reads How we measure 'reads'Author: Merrill Beckstead.
Full text of "Fundamentals Of Solid Propellant Combustion" See other formats. 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.
The main types of liquid propellants are storable propellants, which tend to be hypergolic, and cryogenic propellants. Advantages of liquid propellant.
Liquid-fueled rockets have higher specific impulse than solid rockets and are capable of being throttled, shut down, and restarted.
Only the combustion chamber of a liquid-fueled rocket needs to withstand high combustion pressures. Get this from a library. Combustion of Boron-based Solid Propellants and Solid Fuels: Second International Symposium on Special Topics in Chemical Propulsion. [K Kuo;]. (source: Nielsen Book Data) Summary Reviews state-of-the-art research in the field of combustion of boron-based solid propellants and solid fuels.
The book includes chapters on processing technology and chemical kinetics of boron particles and boron based solid fuels, and combustion of boron particle clouds.
(source: Nielsen Book Data). Reviews state-of-the-art research in the field of combustion of boron-based solid propellants and solid fuels.
The book includes chapters on processing technology and chemical kinetics of boron particles and boron based solid fuels, and combustion of boron particle clouds.Nonsteady Burning and Combustion Stability of Solid Propellants Ingenieria de transportes y aeronautica Volume of Progress in astronautics and aeronautics: Editors: Luigi De Luca, Martin Summerfield: Publisher: AIAA, ISBN:Length: pages: Export Citation: BiBTeX EndNote RefMan.A liquid-propellant rocket or liquid rocket utilizes a rocket engine that uses liquid s are desirable because their reasonably high density allows the volume of the propellant tanks to be relatively low, and it is possible to use lightweight centrifugal turbopumps to pump the propellant from the tanks into the combustion chamber, which means that the .