Pressurization Systems for Liquid Rockets PDF Download
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 180
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Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 180
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Book Description
Author: H. J. Ellis
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 156
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Book Description
Author: Alessandro de Iaco Veris
Publisher: Springer Nature
ISBN: 3030547043
Category : Technology & Engineering
Languages : en
Pages : 755
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Book Description
This book is intended for students and engineers who design and develop liquid-propellant rocket engines, offering them a guide to the theory and practice alike. It first presents the fundamental concepts (the generation of thrust, the gas flow through the combustion chamber and the nozzle, the liquid propellants used, and the combustion process) and then qualitatively and quantitatively describes the principal components involved (the combustion chamber, nozzle, feed systems, control systems, valves, propellant tanks, and interconnecting elements). The book includes extensive data on existing engines, typical values for design parameters, and worked-out examples of how the concepts discussed can be applied, helping readers integrate them in their own work. Detailed bibliographical references (including books, articles, and items from the “gray literature”) are provided at the end of each chapter, together with information on valuable resources that can be found online. Given its scope, the book will be of particular interest to undergraduate and graduate students of aerospace engineering.
Author: Dieter K. Huzel
Publisher: AIAA
ISBN: 9781600864001
Category : Liquid propellant rocket engines
Languages : en
Pages : 452
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Book Description
Author: Josette Bellan
Publisher:
ISBN: 9781624105807
Category : Fluid dynamics (Space environment)
Languages : en
Pages : 0
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Book Description
Describes observations and modelling of high-pressure flows encountered in aeronautics and astronautics. They have been selected to present the current understanding of high-pressure flows. Experimental, theoretical and numerical studies are all represented. Fundamental investigations are presented first, followed by practical studies.
Author: DP Mishra
Publisher: CRC Press
ISBN: 1351708414
Category : Technology & Engineering
Languages : en
Pages : 364
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Book Description
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.
Author: Virginia Parker Dawson
Publisher:
ISBN:
Category : Centaur rocket
Languages : en
Pages : 310
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Book Description
Author: W. A. Wagner
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 172
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Book Description
Author: R. E. Burcham
Publisher:
ISBN:
Category : Fuel pumps
Languages : en
Pages : 192
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Book Description
Author: National Research Council
Publisher: National Academies Press
ISBN: 0309102472
Category : Technology & Engineering
Languages : en
Pages : 288
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Book Description
Rocket and air-breathing propulsion systems are the foundation on which planning for future aerospace systems rests. A Review of United States Air Force and Department of Defense Aerospace Propulsion Needs assesses the existing technical base in these areas and examines the future Air Force capabilities the base will be expected to support. This report also defines gaps and recommends where future warfighter capabilities not yet fully defined could be met by current science and technology development plans.
