Ignition and Unsteady Combustion of AP-based Composite Propellants on Subscale Solid Rocket Motors with Nozzle Seal PDF Download
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Author: A. Bizot
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
Author: A. Bizot
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
Author: A. Bizot
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: Leonard H. Caveny
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
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Book Description
The research carried out under the grant was aimed at furthering the scientific understanding of nonsteady propellant combustion behavior in rocket motor chambers. Controlled nonsteady flow and burning conditions were produced in laboratory-scale solid rocket motors by developing a device that modulated the throat area of the primary nozzle. Modulation frequencies up to 2400 Hz were obtained. The modulated throat rocket motor is being used to acquire data using AP composite propellant grains. Cold flow tests were used to study the acoustic modes and nozzle discharge characteristics. Computerized techniques were developed for conducting spectral analyses of head-end and nozzle-end pressure data. In addition, the equations describing the nonsteady one-dimensional gas dynamics and propellant combustion were formulated, and a comprehensive numerical solution was developed. The present solution takes into account the couplings among the oscillating nozzle flow, the nonsteady chamber flow, and erosive burning. Since pressure and velocity oscillations can be made to occur and decay in high loading density rocket motors with realistic grain configurations, the experiment is expected to produce propellant/chamber response functions that are relatively easy to interpret, compared to the difficult to interpret T-burner response functions.
Author: Martin Summerfield
Publisher: Elsevier
ISBN: 0323163351
Category : Science
Languages : en
Pages : 713
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Book Description
Solid Propellant Rocket Research
Author: Martin Summerfield
Publisher: AIAA
ISBN: 9781600863967
Category : Solid propellants
Languages : en
Pages : 922
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Author: Haridwar Singh
Publisher: Royal Society of Chemistry
ISBN: 1782620966
Category : Science
Languages : en
Pages : 240
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Book Description
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.
Author: Kenneth K. Kuo
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 922
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 684
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Author:
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ISBN:
Category : Airplanes
Languages : en
Pages : 602
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Author: Carlton L. Horine
Publisher:
ISBN:
Category : Solid propellant rockets
Languages : en
Pages : 92
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