2 edition of Solid propellant rocket research found in the catalog.
Solid propellant rocket research
ARS Solid Propellant Rocket Conference (1960 Princeton University)
|Statement||Edited by Martin Summerfield.|
|Series||Progress in astronautics and rocketry,, v. 1|
|Contributions||Summerfield, Martin, ed.|
|LC Classifications||TL507 .P75 vol. 1|
|The Physical Object|
|Pagination||xix, 692 p.|
|Number of Pages||692|
|LC Control Number||60016913|
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. Specific design methods and the theoretical physics. Propellants contain considerable chemical energy that can be used in rocket propulsion. Bringing together information on both the theoretical and practical aspects of solid rocket propellants for the first time, this book will find a unique place on the readers' shelf providing the overall picture of solid rocket propulsion technology. Aimed at students, engineers and researchers in the area.
The space shuttle advanced solid rocket motor: Quality control and testing The Congressional committees that authorize the activities of NASA requested that the National Research Council (NRC) review the testing and quality assurance programs for the Advanced Solid Rocket Motor (ASRM) program. The proposed ASRM design incorporates numerous features that are significant . It became clear that for the mid-range SRMs, the pressure exponent in the burning rate law of solid propellants has to be of low magnitude (around –), and scatter in the values of solid-propellant burning rates has to come closer to the level of deviation for values of other parameters such as density of solid-propellant or design.
In recent times, solid propellant rocket motors have been used in anti-tank weapons, air-to-air and air-to-ground rockets, and intercontinental ballistic missiles, as well as launch vehicles for. Liquid propellant rocket engine developed by Lubbock and Gollin at Langhurst ) and would evolve into the propulsion unit for the Research Test Vehicle 1 (RTV1). In Feburary the construction of the Solid Propellant Laboratories (SPL) development scale rocket motor filling factory commenced and by July the first Solid motor filled (a.
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This volume on Solid Propellant Rocket Research is the first in a new series, Progress in Astronautics and Rocketry, sponsored by the American Rocket Society.
In selecting the papers for the volume, the editor attempted to meet as nearly as possible the present needs of solid rocket research scientists for an up-to-date view of the most.
Purchase Solid Propellant Rocket Research - 1st Edition. Print Book & E-Book. ISBNBook Edition: 1. Current research on the effects of the composition and the physical state of the propellant on both the combustion characteristics and the structural properties is reviewed. a solid propellant rocket motor is a unique structure in that it is composed of a substantial mass of propellant material case-bonded to a relatively massless, thin.
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.
The ignition and combustion property of solid propellant is the main content in internal ballistic research, which has a great significance for propulsion application and combustion mechanism. 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. The scope of this study is to improve combustion performance of a boron-based solid propellant ducted rocket (SPDR).
A numerical approach for the internal reaction flow in SPDR was built, and an. 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 fundamentals of rocket propulsion are developed in chapter one and detailed descriptions of concepts are covered in the following s: 4.
The Space Shuttle Solid Rocket Booster (Space Shuttle SRB) was the first solid-propellant rocket to be used for primary propulsion on a vehicle used for human spaceflight and provided the majority of the Space Shuttle's thrust during the first two minutes of flight.
After burnout, they were jettisoned and parachuted into the Atlantic Ocean where they were recovered, examined, refurbished, and. Dr. Kubota received a Doctorate from Princeton University inmajoring in "Solid Propellant Combustion" and "Rocket Propulsion including Ducted Rocket Engine".
His current position is Senior Research Scientist of Propellant Combustion Laboratory, Asahi Kasei Chemicals. In the fieldof solid rocket propulsion, the few that are available are technical in nature (HS Mukunda, Understanding Aerospace Chemical Propulsion, Interline Publishing, and Haridwar Singh and Himanshu Shekhar, Science and Technology of Solid Rocket Propellants, ); and this book is an attempt to provide the background to.
Much of the research in solid propellants is devoted to improving the physical as well as the chemical properties of the fuel.
Ordinarily, in processing solid propellants the fuel and oxidizer components are separately prepared for mixing, the oxidizer being a powder and the fuel a fluid of varying consistency.
Abstract. The solid-propellant rocket motor brings the flight mission capability of high thrust delivery over a short duration. Design issues, such as tailoring the shape of the solid propellant grain (charge) to produce a desired thrust-time profile, are discussed in some detail in this chapter.
Solid Propellant Rocket Research Vol.1 Paperback – December 3, by Martin Summerfield (Editor) See all 3 formats and editions Hide other formats and editions. Price New from Used from Hardcover "Please retry" $ — $ Format: Paperback.
Genre/Form: Electronic books Congresses: Additional Physical Format: Print version: Summerfield, Martin. Solid Propellant Rocket Research.
Burlington: Elsevier. Each rocket assembly is an integrated system, incorporating a combustion chamber, composite propellant grain, nozzle, igniter, and thermoelectric power con-verter. Solid propellant is advantageous for a millimeter-scale single-use device because of its simple implementation, unlike liquid propellants, which require a more elaborate system of.
Innovative Solid Rocket Propellant Formulations for Space Propulsion: /ch Solid rocket propulsion enjoys unique properties favoring its use in space exploration and military missions still for decades to come.
Yet, it also suffers a. On this slide, we show a schematic of a solid rocket engine. Solid rocket engines are used on air-to-air and air-to-ground missiles, on model rockets, and as boosters for satellite a solid rocket, the fuel and oxidizer are mixed together into a solid propellant which is packed into a solid cylinder.
A hole through the cylinder serves as a combustion chamber. Electronic books Conference papers and proceedings Congresses: Additional Physical Format: Print version: ARS Solid Propellant Rocket Conference ( Princeton University).
Solid propellant rocket research. New York: Academic Press, (DLC) Material Type: Conference publication, Document, Internet resource: Document Type. The objective of the book is twofold, first to present basic material on solid propellant rockets which can be used for classroom instruction and second to carry the reader to the frontiers of research in a number of specific areas of solid propellant rocketry.
Although there is some material which might appropriately be used in undergraduate courses, the instructional value of the book lies. In he received his Doctorate from Princeton University, majoring in "Solid Propellant Combustion" and "Rocket Propulsion including Ducted Rocket Engine".
During his career he was Director of the Third Research Center of the Technical Research and Development Institute (TRDI, Japan Defense Agency), which is responsible for aircraft and.Terry McCreary's book EXPERIMENTAL COMPOSITE PROPELLANTS was a success right out of the gate when it was first published in the year It has become THE Bible for today's Research Rocketry enthusiasts.
Written addressing P-Ban based propellants it's content is more encompassing to all rocket propellants and the knowledge presented on the how's and why's is applicable to all solid.Nanomaterials in Rocket Propulsion Systems covers the fundamentals of nanomaterials and examines a wide range of innovative applications, presenting the current state-of-the-art in the g with a chapter on nano-sized energetic materials, the book examines metal nanoparticles-based fuels, ballistic modifiers, stabilizers and catalysts as the components of rocket propellants.