Solid Propellant Grain Structural Integrity Analysis PDF Download

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State of the Art of Solid Propellant Rocket Motor Grain Design in the United States

State of the Art of Solid Propellant Rocket Motor Grain Design in the United States
Author: Durwood I. Thrasher
Publisher:
Total Pages: 21
Release: 1988
Genre:
ISBN:

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This paper begins with a brief discussion of the basic ground rules and overall considerations in solid rocket motor design. This discussion includes ballistic design considerations, grain features related to ballistic design and their purposes, primary factors which determine stress and strain levels, and design approaches for avoiding structural weak points. The major section of the paper deals with solid rocket motor propellant grain structural integrity assurance, including materials characterization, structural analysis, and structural capability verification. The topics addressed include viscoelastic material behavior and the requisite thermomechanical characterization testing and analysis approaches; failure criteria and the appropriate testing approaches; experimental structural methods, including in-situ stress and strain measurement technology; and service life considerations.


Quick-Look Structural Analysis Techniques for Solid Rocket Propellant Grains

Quick-Look Structural Analysis Techniques for Solid Rocket Propellant Grains
Author: Russell A. Leighton
Publisher:
Total Pages: 47
Release: 1982
Genre:
ISBN:

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Software was developed to provide the means to perform a 'quick-look' preliminary motor structural analysis within the AFRPL. Preliminary structural analysis equations from the JANNAF Structural Integrity Handbook and Galcit 101, 'Fundamental Studies Relating to Systems Analyses of Solid Propellants' were implemented on the HP 9815A programmable calculator as a basis for the software. For analysis of a motor undergoing a thermal transient load, software was written to provide the means to calculate an effective modulus, based on linear viscoelastic theory, for use in the 'quick-look' analysis. Supporting software was also written to provide graphical input of data and to correct any distortions appearing in supplied data. Finally, results from a simple, slow cooldown problem were obtained from a finite element analysis using the TEXGAP 2D computer code to verify the usefulness and accuracy of the 'quick-look' analysis and supporting software.


Mechanics and Chemistry of Solid Propellants

Mechanics and Chemistry of Solid Propellants
Author: A. C. Eringen
Publisher: Elsevier
Total Pages: 648
Release: 2014-06-28
Genre: Technology & Engineering
ISBN: 148322340X

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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.


Solid Rocket Propulsion Technology

Solid Rocket Propulsion Technology
Author: A. Davenas
Publisher: Newnes
Total Pages: 623
Release: 2012-12-02
Genre: Technology & Engineering
ISBN: 0080984754

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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 underlying them are presented, and finally the industrial production of the propellant itself is explained. The material used in the book has been collected from different countries, as the development of this field has occurred separately due to the classified nature of the subject. Thus the reader not only has an overall picture of solid rocket propulsion technology but a comprehensive view of its different developmental permutations worldwide.