An Investigation Into the Mechanisms of Combustion of a Double-base Solid Propellant PDF Download
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Author: Charley Lewis Thompson
Publisher:
ISBN:
Category : Solid propellants
Languages : en
Pages : 250
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Book Description
Author: Charley Lewis Thompson
Publisher:
ISBN:
Category : Solid propellants
Languages : en
Pages : 250
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Book Description
Author: Cecil Eugene Kirby
Publisher:
ISBN:
Category : Calorimeters
Languages : en
Pages : 36
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Book Description
Heat of reaction for flameless combustion of M-2 double-base propellant /20 percent nitroglycerin 77 percent nitrocellulose, 3 percent other ingredients/ at varying pressures.
Author: Naminosuke Kubota
Publisher: John Wiley & Sons
ISBN: 3527693513
Category : Science
Languages : en
Pages : 560
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Book Description
This third edition of the classic on the thermochemical aspects of the combustion of propellants and explosives is completely revised and updated and now includes a section on green propellants and offers an up-to-date view of the thermochemical aspects of combustion and corresponding applications. 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. Finally, an appendix gives a brief overview of the fundamentals of aerodynamics and heat transfer, which is a prerequisite for the study of pyrodynamics. A detailed reference for readers interested in rocketry or explosives technology.
Author: Guy Lengellae
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
Author: Vigor Yang
Publisher: AIAA
ISBN: 9781600864377
Category : Ballistics, Interior
Languages : en
Pages : 1038
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Book Description
Author: Brian Elliott Davis
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
Author: Cecil Eugene Kirby
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
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Book Description
Author: Martin Summerfield
Publisher: Elsevier
ISBN: 0323163351
Category : Science
Languages : en
Pages : 713
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Book Description
Solid Propellant Rocket Research
Author: Clayton Huggett
Publisher: Princeton University Press
ISBN: 1400879078
Category : Science
Languages : en
Pages : 175
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Book Description
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.
Author: M. Summerfield
Publisher:
ISBN:
Category :
Languages : en
Pages : 15
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Book Description
The annual report highlights the progress being made on several concurrent solid propellant combustion mechanism researches. Studies of nitrocellulose-base propellants have produced a broad range of experimental results for platonized and unplatonized propellants. The corresponding mathematical models consider the flame zone processes controlling temperature sensitivity, extinguishment limits, and burning rate. The analytical studies of ignition and burning of porous propellants are producing good agreement with data, new insights into the combustion processes, and establishing regimes where steady-state burning rates are achievable. The work of nonsteady burning has progressed to the point that rocket motor transients can be predicted and dynamic burning rates in a variable throat area, low L* motor can be measured; this work has progressed from the research phase to the development stage. Sub- micron pyrophoric aluminum is being investigated as a means of increasing propellant burning rate.
