Principles of Nuclear Rocket Propulsion, Emrich, Jr., William J.
Новое издание
Автор: Emrich, Jr., William J. (senior Engineer, Nasa/marshall Space Flight Center, Huntsville, Al, Usa (retired) And Adjunct Professor, University Of Alabam Название: Principles of nuclear rocket propulsion ISBN: 0323900305 ISBN-13(EAN): 9780323900300 Издательство: Elsevier Science Цена: 22065.00 р. Наличие на складе: Есть у поставщикаПоставка под заказ.
Автор: Martin J. L. Turner Название: Rocket and Spacecraft Propulsion ISBN: 3642088694 ISBN-13(EAN): 9783642088698 Издательство: Springer Рейтинг: Цена: 22201.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: The revised third edition of this eminently practical, hands-on book discusses the range of launch vehicles in use today throughout the world, and includes the very latest details of some of the advanced propulsion systems currently being developed.
Автор: Cumpsty Название: Jet Propulsion ISBN: 1107511224 ISBN-13(EAN): 9781107511224 Издательство: Cambridge Academ Рейтинг: Цена: 7918.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: This book is a self-contained introduction to the design of modern civil and military jet engines through two-engine design projects for a large passenger and a new fighter aircraft. Numerous exercises, with solutions for the instructor, are included. The book emphasizes principles enriched by industrial examples from the author`s experience.
Автор: Sforza, Pasquale M Название: Theory of Aerospace Propulsion ISBN: 0128093269 ISBN-13(EAN): 9780128093269 Издательство: Elsevier Science Рейтинг: Цена: 14820.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание:
Theory of Aerospace Propulsion, Second Edition, teaches engineering students how to utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines, understand the common gas turbine aircraft propulsion systems, be able to determine the applicability of each, perform system studies of aircraft engine systems for specified flight conditions and preliminary aerothermal design of turbomachinery components, and conceive, analyze, and optimize competing preliminary designs for conventional and unconventional missions. This updated edition has been fully revised, with new content, new examples and problems, and improved illustrations to better facilitate learning of key concepts.
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