Impulse of Reactive Force of Solid Propellant Rockets

Impulse of Reactive Force of Solid Propellant Rockets
Author: Ya B. Zeldovich
Publisher:
Total Pages: 194
Release: 1966
Genre:
ISBN:

The book is devoted to thermodynamic theory of calculating the impulse of reactive force of a solid propellant rocket. In it there is presented the thermodynamics of powder gases, thermodynamic calculation of a solid propellant rocket, methods of measurement of specific impulse and calculation of its magnitude for powders of different caloric value. Consideration is given to heat transfer in a solid propellant rocket, the influence of conditions of ignition of the propellant on the magntiude of the specific impulse, reasons for scattering of the magnitude of the specific impulse and methods of measuring this scattering, and the efflux coefficient. The book is designed for scientists and engineers, specializing in the area of rocket technology. (Soviet editor's note).

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

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.

Solid Rocket Propellants

Solid Rocket Propellants
Author: Haridwar Singh
Publisher: Royal Society of Chemistry
Total Pages: 183
Release: 2019-03-07
Genre: Technology & Engineering
ISBN: 1788018087

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 authors have applied their wealth of knowledge regarding formulation, processing and evaluation to provide an up to date and clear text on the subject.

Fundamentals of Rocket Propulsion

Fundamentals of Rocket Propulsion
Author: DP Mishra
Publisher: CRC Press
Total Pages: 364
Release: 2017-07-20
Genre: Technology & Engineering
ISBN: 1351708414

The book follows a unified approach to present the basic principles of rocket propulsion in concise and lucid form. This textbook comprises of ten chapters ranging from brief introduction and elements of rocket propulsion, aerothermodynamics to solid, liquid and hybrid propellant rocket engines with chapter on electrical propulsion. Worked out examples are also provided at the end of chapter for understanding uncertainty analysis. This book is designed and developed as an introductory text on the fundamental aspects of rocket propulsion for both undergraduate and graduate students. It is also aimed towards practicing engineers in the field of space engineering. This comprehensive guide also provides adequate problems for audience to understand intricate aspects of rocket propulsion enabling them to design and develop rocket engines for peaceful purposes.

Solid Propellant Rockets

Solid Propellant Rockets
Author: Clayton Huggett
Publisher: Princeton University Press
Total Pages: 175
Release: 2015-12-08
Genre: Science
ISBN: 1400879078

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.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Author:
Publisher:
Total Pages: 1126
Release: 1987
Genre: Aeronautics
ISBN:

Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.