Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 180
Book Description
Pressurization Systems for Liquid Rockets
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 180
Book Description
Liquid Rocket Valve Components
Author: H. J. EllisPublisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 156
Book Description
Pressurization Systems Design Guide: pt.A-B. Design procedures and data
Author: Aerojet-General CorporationPublisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 458
Book Description
Modern Engineering for Design of Liquid-Propellant Rocket Engines
Author: Dieter K. HuzelPublisher: AIAA
ISBN: 9781600864001
Category : Liquid propellant rocket engines
Languages : en
Pages : 452
Book Description
Fundamental Concepts of Liquid-Propellant Rocket Engines
Author: Alessandro de Iaco VerisPublisher: Springer Nature
ISBN: 3030547043
Category : Technology & Engineering
Languages : en
Pages : 747
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.
High-pressure Flows for Propulsion Applications
Author: Josette BellanPublisher:
ISBN: 9781624105807
Category : Fluid dynamics (Space environment)
Languages : en
Pages : 0
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.
Fundamentals of Rocket Propulsion
Author: DP MishraPublisher: CRC Press
ISBN: 1351708414
Category : Technology & Engineering
Languages : en
Pages : 364
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.
Taming Liquid Hydrogen
Author: Virginia Parker DawsonPublisher:
ISBN:
Category : Centaur rocket
Languages : en
Pages : 310
Book Description
Liquid Propellant Rocket Combustion Instability
Author: David T. HarrjePublisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 668
Book Description
The solution of problems of combustion instability for more effective communication between the various workers in this field is considered. The extent of combustion instability problems in liquid propellant rocket engines and recommendations for their solution are discussed. The most significant developments, both theoretical and experimental, are presented, with emphasis on fundamental principles and relationships between alternative approaches.
Liquid Rocket Metal Tanks and Tank Components
Author: W. A. WagnerPublisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 172
Book Description