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Soyuz / A Universal Spacecraft, Hall Rex, Shayler David



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Цена: 4179р.
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Склад Англия: 405 шт.  Склад Америка: 88 шт.  
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Автор: Hall Rex, Shayler David
Название:  Soyuz / A Universal Spacecraft
Перевод названия: Рекс Холл: Союз. Универсальный космический корабль
ISBN: 9781852336578
Издательство: Springer
Классификация:
ISBN-10: 1852336579
Обложка/Формат: Paperback
Страницы: 495
Вес: 0.932 кг.
Дата издания: 07.05.2003
Серия: Springer Praxis Books / Space Exploration
Язык: English
Издание: Twenty-eighth
Иллюстрации: Illustrations, glossary, references, bibliography,
Размер: 252 x 180 x 26
Читательская аудитория: Postgraduate, research & scholarly
Подзаголовок: A universal spacecraft
Ссылка на Издательство: Link
Рейтинг:
Поставляется из: Германии
Дополнительное описание: Формат: 242x170
Круг читателей: Space enthusiasts
Ключевые слова: Universal spacecraft
Soviet Moon Programme and Space Technology
Язык: eng
Оглавление: Foreword.- Author's Introduction.- Preface: Into Space on Soyuz.- Origins.- Early Soyuz.- First Flights.- The Lunar Adventure.- Return to Flight.- Soyuz to Salyut.- Solo Soyuz.- 3-Person Upgrade.- Space Freighter.- Soyuz for ISS.- Cosmonaut Training.- Unmanned Applications.- Appendices.- Glossary.- References.- Bibliography.- Index.





Transistor Circuits for Spacecraft Power System

Автор: Wu Keng C.
Название: Transistor Circuits for Spacecraft Power System
ISBN: 1402072619 ISBN-13(EAN): 9781402072611
Издательство: Springer
Рейтинг:
Цена: 17578 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Описание: As a stand-alone volume, Transistor Circuits For Spacecraft Power System presents numerous transistor circuits and building blocks associated with power electronics in general, and examines the major subsystem components for solar-based spacecraft power systems. The technique and concept, of "continuity of states" for nonlinear circuits handling power transfer under cyclic excitation is introduced in Part I and further developed throughout the book. This powerful technique employing matrix formulation bypasses eigen-transients and yields steady-state responses rapidly. Closed-loop treatments are also given for large-scale linear circuits, many closed-form solutions for control loop-gain, conducted susceptibility, output impedance, etc. are covered. Extensive mathematical procedures are retained to highlight the importance of analytical flows.The author also reviews the evolution of solar-based spacecraft power systems; introduces modes of operations: discharge (boost), shunt, and charge; and covers pulse-width-modulated (PWM) boost power converter for both DC and AC conditions. A configuration tree for shunt mode operation is conceived. Based on the configuration tree, the best topologies, sequential PWM shunt and ripple-regulated free-running shunt, are intensively examined and formulated.Transistor Circuits For Spacecraft Power System provides important information for understanding the relationship between earthbound semiconductor circuits and space borne vehicles.

Future Spacecraft Propulsion Systems / Enabling Technologies for Space Exploration

Автор: Czysz Paul A., Bruno Claudio
Название: Future Spacecraft Propulsion Systems / Enabling Technologies for Space Exploration
ISBN: 3540231617 ISBN-13(EAN): 9783540231615
Издательство: Springer
Цена: 14625 р.
Наличие на складе: Поставка под заказ.

Описание: In Future Spacecraft Propulsion Systems the authors demonstrate the need to break free from the old established concepts of expendable rockets, using chemical propulsion, and to develop new breeds of launch vehicle capable of both launching payloads into orbit at dramatically reduced cost, and for sustained operations in low-Earth orbit. The next steps, they explain, to establishing a permanent "presence" in the solar system beyond Earth are the commercialisation of sustained operations on the Moon, and the development of advanced nuclear or high-energy space propulsion systems for solar system exploration out to the boundary of interstellar space. In the future, high-energy particle research facilities may one day yield a very high-energy propulsion system that will take us to the nearby stars, or even beyond. This is a timely and comprehensive book, putting spacecraft propulsion systems in perspective.

Spacecraft reliability and multi-state failures

Автор: Saleh, Joseph Homer Castet, Jean-francois
Название: Spacecraft reliability and multi-state failures
ISBN: 0470687916 ISBN-13(EAN): 9780470687918
Издательство: Wiley
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Цена: 12012 р.
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Описание: * Unique focus on spacecraft and satellite reliability based on statistical analysis of mission failures and successes.

Spacecraft Power Systems

Автор: Patel
Название: Spacecraft Power Systems
ISBN: 0849327865 ISBN-13(EAN): 9780849327865
Издательство: Taylor&Francis
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Цена: 24255 р.
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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.

The Soyuz Launch Vehicle

Автор: Lardier
Название: The Soyuz Launch Vehicle
ISBN: 1461454581 ISBN-13(EAN): 9781461454588
Издательство: Springer
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Цена: 4882 р.
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Описание: This authoritative chronicle of the 1950s gestation and modern reanimation of the Soyuz launcher details innumerable aspects of the history, including the measures taken by the Soviets to disguise their work on rocketry and the system`s recent commercial use.

Spacecraft Attitude Determination and Control

Автор: Wertz
Название: Spacecraft Attitude Determination and Control
ISBN: 9027712042 ISBN-13(EAN): 9789027712042
Издательство: Springer
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Цена: 22989 р.
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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.

Spacecraft Systems Engineering, 3rd Edition

Автор: Peter Fortescue, John Stark
Название: Spacecraft Systems Engineering, 3rd Edition
ISBN: 0470851023 ISBN-13(EAN): 9780470851029
Издательство: Wiley
Цена: 10395 р.
Наличие на складе: Поставка под заказ.

Описание: Encompassing the fundamentals of spacecraft engineering, this book begins with front end system level issues, such as environment, mission analysis and system engineering, and progresses to a detailed examination of subsystem elements which represent the core of spacecraft design mechanical, electrical, propulsion, thermal, and control.

Automated Rendezvous and Docking of Spacecraft

Автор: Fehse
Название: Automated Rendezvous and Docking of Spacecraft
ISBN: 0521089867 ISBN-13(EAN): 9780521089869
Издательство: Cambridge Academ
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Цена: 9317 р.
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Описание: The definitive reference for space engineers on all issues related to rendezvous and docking/berthing (RVD/B).

Mechanical Vibrations in Spacecraft Design

Автор: Wijker Jaap
Название: Mechanical Vibrations in Spacecraft Design
ISBN: 3540405305 ISBN-13(EAN): 9783540405306
Издательство: Springer
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Цена: 13672 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Описание: All typical and special modal and response analysis methods, applied within the frame of the design of spacecraft structures, are described in this book. It therefore addresses graduate students and engineers in the aerospace field.

Spacecraft Systems Engineering, 3rd Edition

Автор: Peter Fortescue
Название: Spacecraft Systems Engineering, 3rd Edition
ISBN: 0471619515 ISBN-13(EAN): 9780471619512
Издательство: Wiley
Рейтинг:
Цена: 4614 р.
Наличие на складе: Поставка под заказ.

Описание: The material in this book is essential for engineers studying and working in the field of spececraft design. The unique feature of this book is that its coverage aims at giving the breadth which is needed by system engineers, with an emphasis on the bus aspect rather than on the payload. This second edition is an updated of the first, and includes two estra chapters. The first is on Mechanisms, and the second is on the subhject of Systems Engineering, and it includes examples of applications to different types of missions.

Mission Geometry; Orbit and Constellation Design and Management / Spacecraft Orbit and Attitude Systems

Автор: Wertz J.R.
Название: Mission Geometry; Orbit and Constellation Design and Management / Spacecraft Orbit and Attitude Systems
ISBN: 0792371488 ISBN-13(EAN): 9780792371489
Издательство: Springer
Рейтинг:
Цена: 24034 р.
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Описание: Mission Geometry; Orbit and Constellation Design and Management (OCDM) is the most complete treatment available for many elements of space mission design and astronautics. Among these topics not covered elsewhere in the literature are:

  • The most extensive coverage available of constellation design and management;
  • Relative motion of satellites (global, local, at similar and widely differing altitudes);
  • Definition of an Orbit Cost Function for comparing the cost of access to and maintenance of alternative orbits;
  • Most extensive discussions available of autonomous navigation and autonomous orbit control;
  • The most complete discussion available of Earth coverage and viewing and lighting conditions;
  • Apparent motion of other satellites needed for cross-link pointing and antenna coverage;
  • Analytic expressions for the field of view of an array processor on the celestial sphere and projected onto the Earth's surface;
  • Detailed process for creating and analyzing mapping, pointing, and timing budgets;
  • Closed-form expressions for the ground track of a circular orbit, including high accuracy approximations for ground station coverage;
  • Convenient formulas for specialized orbits about the Earth and other planets;
  • Practical spacecraft problems such as time discontinuities, GPS coverage at satellite altitudes, and how to identify and handle singularities in measurement sets; and
  • New solutions for all possible spherical triangles without quadrant ambiguities and allowing all sides and angles to range from 0 to 360 deg.

OCDM discusses both the similarities and differences between orbit and altitude systems in terms of hardware, algorithms, design, and processing requirements. With the demand for reduced cost and the introduction of extensive on-board computing, what were once entirely separate disciplines have begun to merge. This volume will speed that process.

In all areas, OCDM is meant to be practical, with recommendations, insights, formulas, and numerical recipes based on 40 years of spaceflight experience from organizations worldwide. It is meant to be both a text and reference work that can be used by those entering the field and by senior engineers engaged in the design, analysis, construction, or on-orbit operations of orbit and attitude systems and components.

Copyright Microcosm: www.smad.com

Spacecraft Trajectory Optimization

Автор: Conway
Название: Spacecraft Trajectory Optimization
ISBN: 0521518504 ISBN-13(EAN): 9780521518505
Издательство: Cambridge Academ
Рейтинг:
Цена: 11388 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Описание: This is a long-overdue volume dedicated to space trajectory optimization. Interest in the subject has grown, as space missions of increasing levels of sophistication, complexity, and scientific return - hardly imaginable in the 1960s - have been designed and flown. Although the basic tools of optimization theory remain an accepted canon, there has been a revolution in the manner in which they are applied and in the development of numerical optimization. This volume purposely includes a variety of both analytical and numerical approaches to trajectory optimization. The choice of authors has been guided by the editor's intention to assemble the most expert and active researchers in the various specialities presented. The authors were given considerable freedom to choose their subjects, and although this may yield a somewhat eclectic volume, it also yields chapters written with palpable enthusiasm and relevance to contemporary problems.


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