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|n Title subscribed to via ProQuest Academic Complete
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|a dlr
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|a TL875
|b .B76 2002
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|a 629.47
|2 21
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|a UAMI
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100 |
1 |
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|a Brown, Charles D.,
|d 1930-
|1 https://id.oclc.org/worldcat/entity/E39PCjygb3cvJRXMkgqDqXHCry
|
245 |
1 |
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|a Elements of spacecraft design /
|c Charles D. Brown.
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260 |
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|a Reston, VA :
|b American Institute of Aeronautics and Astronautics,
|c ©2002.
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300 |
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|a 1 online resource (xi, 610 pages) :
|b illustrations
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336 |
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|a text
|b txt
|2 rdacontent
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|a computer
|b c
|2 rdamedia
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|a online resource
|b cr
|2 rdacarrier
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|a data file
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|a AIAA education series
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504 |
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|a Includes bibliographical references and index.
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520 |
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|a Annotation
|b This text discusses the conceptual stages of mission design, systems engineering, and orbital mechanics, providing a basis for understanding the design process for different components and functions of a spacecraft. Coverage includes propulsion and power systems, structures, attitude control, thermal control, command and data systems, and telecommunications. Worked examples and exercises are included, in addition to appendices on acronyms and abbreviations and spacecraft design data. The book can be used for self-study or for a course in spacecraft design. Brown directed the team that produced the Magellan spacecraft, and has taught spacecraft design at the University of Colorado. Annotation c. Book News, Inc., Portland, OR (booknews.com).
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520 |
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|a Annotation
|b This new book is drawn from the author's years of experience in spacecraft design, culminating in his leadership of the Magellan Venus orbiter spacecraft design from concept through launch. The book also benefits from his years of teaching spacecraft design at University of Colorado at Boulder and as a popular home study short course for AIAA. The book presents a broad view of the complete spacecraft. The objective is to explain the thought and analysis that go into the creation of a spacecraft with simplicity and with enough worked examples so that the reader can be self taught if necessary. After studying the book, readers should be able to design a spacecraft, to the phase A level, by themselves Everyone who works in or around the spacecraft industry should know this much about the entire machine.
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|a Print version record.
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|3 Use copy
|f Restrictions unspecified
|2 star
|5 MiAaHDL
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|a Electronic reproduction.
|b [Place of publication not identified] :
|c HathiTrust Digital Library,
|d 2010.
|5 MiAaHDL
|
538 |
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|a Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.
|u http://purl.oclc.org/DLF/benchrepro0212
|5 MiAaHDL
|
583 |
1 |
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|a digitized
|c 2010
|h HathiTrust Digital Library
|l committed to preserve
|2 pda
|5 MiAaHDL
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0 |
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|a Cover -- Title -- Copyright -- Foreword -- Table of Contents -- Chapter 1. Introduction -- 1.1 First Spacecraft -- 1.2 Spacecraft Missions -- References -- Chapter 2. System Engineering -- 2.1 Anatomy of a Spacecraft -- 2.2 Mass Properties -- 2.3 Power -- 2.4 Other Margins -- 2.5 Redundancy Techniques -- 2.6 Launch Vehicle Interface -- References -- Problems -- Chapter 3. Orbital Mechanics -- 3.1 Two-Body Motion -- 3.2 Orbital Maneuvers -- 3.3 Observing the Central Body -- 3.4 Special Earth Orbits -- 3.5 Interplanetary Trajectories
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|a 3.6 Lunar TrajectoriesReferences -- Problems -- Chapter 4. Propulsion -- 4.1 Introduction -- 4.2 Theoretical Rocket Performance -- 4.3 Propulsion Requirements -- 4.4 Monopropellant Systems -- 4.5 Bipropellant Systems -- 4.6 Dual-Mode Systems -- 4.7 Solid Rocket Systems -- 4.8 Cold-Gas Systems -- References -- Problems -- Chapter 5. Attitude Control -- 5.1 Requirements Definition -- 5.2 Disturbance Torques -- 5.3 Attitude Determination -- 5.4 Attitude Control Systems -- 5.5 Maneuver Design -- 5.6 Attitude Control Hardware -- References
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|a ProblemsChapter 6. Power System -- 6.1 Power System Requirements -- 6.2 Solar Arrays -- 6.3 Radioisotope Thermoelectric Generators -- 6.4 Batteries -- 6.5 Power Distribution and Control -- 6.6 Estimating Subsystem Mass -- References -- Problems -- Chapter 7. Thermal Control -- 7.1 Relationship to Other Subsystems -- 7.2 General Approaches and Options -- 7.3 General Design Methodology -- 7.4 Basic Analytical Equations and Relations -- 7.5 Preliminary Design -- 7.6 Preliminary Design Process -- 7.7 Thermophysical Properties -- 7.8 Design Considerations
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|a 10.3 Structure Design10.4 Mechanisms -- References -- Problems -- Appendix A. Acronyms and Abbreviations -- Appendix B. Spacecraft Design Data -- Index -- A -- B -- C -- D -- E -- F -- G -- H -- I -- J -- K -- L -- M -- N -- O -- P -- Q -- R -- S -- T -- U -- V -- W -- Z
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546 |
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|a English.
|
590 |
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|a ProQuest Ebook Central
|b Ebook Central Academic Complete
|
650 |
|
0 |
|a Space vehicles
|x Design and construction.
|
650 |
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6 |
|a Véhicules spatiaux
|x Conception et construction.
|
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|a Space vehicles
|x Design and construction
|2 fast
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655 |
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7 |
|a dissertations.
|2 aat
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|a Academic theses
|2 fast
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|a Academic theses.
|2 lcgft
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|a Thèses et écrits académiques.
|2 rvmgf
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|i has work:
|a Elements of spacecraft design (Text)
|1 https://id.oclc.org/worldcat/entity/E39PCFTxKTWrGc6jWr7cKDwPV3
|4 https://id.oclc.org/worldcat/ontology/hasWork
|
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|i Print version:
|a Brown, Charles D., 1930-
|t Elements of spacecraft design.
|d Reston, VA : American Institute of Aeronautics and Astronautics, ©2002
|w (DLC) 2002010232
|w (OCoLC)50114369
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|a AIAA education series.
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