Spacecraft Structures and Mechanisms, Sarafin

Автор: Hall Rex, Shayler David
Название: Soyuz / A Universal Spacecraft
ISBN: 1852336579 ISBN-13(EAN): 9781852336578
Издательство: Springer
Рейтинг:
Цена: 46570.00 T
Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Rex Hall and Dave Shayler provide a unique history of the Soyuz spacecraft programme from conception, through development to its use, detailed in the only English language book available on this topic. Planned for publication in 2003, it will celebrate 40 years since the original concept of the Soyuz craft.

Автор: Martin J. L. Turner
Название: Rocket and Spacecraft Propulsion
ISBN: 3642088694 ISBN-13(EAN): 9783642088698
Издательство: Springer
Рейтинг:
Цена: 148010.00 T
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: Patel
Название: Spacecraft Power Systems
ISBN: 0849327865 ISBN-13(EAN): 9780849327865
Издательство: Taylor&Francis
Рейтинг:
Цена: 234790.00 T
Наличие на складе: Поставка под заказ.
Описание: Presents information on the various aspects of spacecraft power system design, analysis, and operation for various types of spacecrafts: earth-orbiting, interplanetary, and deep-space. This work presents modern data and procedures for designing electrical power systems that meet mission requirements at a minimum cost and weight.

Автор: Wertz
Название: Spacecraft Attitude Determination and Control
ISBN: 9027712042 ISBN-13(EAN): 9789027712042
Издательство: Springer
Рейтинг:
Цена: 204970.00 T
Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: A comprehensive presentation of data, theory and practice in attitude analysis. It features discussions of common data anomalies, data validation, attitude hardware and associated mathematical models, and a presentation of geometrical procedures for mission analysis and attitude accuracy studies which can eliminate many complex simulations.