Final Report on Ignition and Combustion of Solid Propellants PDF Download
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Author: University of Utah. Department of Chemical Engineering
Publisher:
ISBN:
Category : Solid propellants
Languages : en
Pages :
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Book Description
Author: University of Utah. Department of Chemical Engineering
Publisher:
ISBN:
Category : Solid propellants
Languages : en
Pages :
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Book Description
Author: Rex C. Mitchell
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 152
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Book Description
The original objective of this project was to study the ignition of composite propellants. It was broadened to encompass the study of other combustion transients, these being, so far, subjected only to exploratory investigation.
Author: Martin Summerfield
Publisher: Elsevier
ISBN: 0323163351
Category : Science
Languages : en
Pages : 713
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Book Description
Solid Propellant Rocket Research
Author: John A. Keller
Publisher:
ISBN:
Category :
Languages : en
Pages : 72
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Book Description
A report is given of work in the following areas: ignition theory, ignition of propellants by high convective heat fluxes, hot-wire ignition, fuel-binder decomposition studies, and propellant extinguishment.
Author: K. K. Kuo
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
Author: Martin Summerfield
Publisher: AIAA
ISBN: 9781600863967
Category : Solid propellants
Languages : en
Pages : 922
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Book Description
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.
Author: Leonard Dauerman
Publisher:
ISBN:
Category :
Languages : en
Pages : 15
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Book Description
This final report summarizes work in the following areas: (1) Applications of tandem strand burner - mass spectrometer technique; (2) Development and applications of tandem strans burner - IR-UV-visible spectrometer technique; (3) Development and application of multiple internal reflectance spectroscopy to the study of surface reactions; (4) A mechanism proposed to explain the activity of catalysts in composite propellants. (Author).
Author: Harrison Allen
Publisher:
ISBN:
Category : Chlorine trifluoride
Languages : en
Pages : 28
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Book Description
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.
