Structural Design Criteria Applicable to a Space Shuttle
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Page : 112 pages
File Size : 34,63 MB
Release : 1972
Category : Reusable space vehicles
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Author :
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Page : 112 pages
File Size : 34,63 MB
Release : 1972
Category : Reusable space vehicles
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Page : 68 pages
File Size : 46,15 MB
Release : 1971
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Page : 92 pages
File Size : 28,59 MB
Release : 1971
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Author : B.N. Suresh
Publisher : Springer
Page : 792 pages
File Size : 40,58 MB
Release : 2015-11-20
Category : Technology & Engineering
ISBN : 8132225325
The book addresses the overall integrated design aspects of a space transportation system involving several disciplines like propulsion, vehicle structures, aerodynamics, flight mechanics, navigation, guidance and control systems, stage auxiliary systems, thermal systems etc. and discusses the system approach for design, trade off analysis, system life cycle considerations, important aspects in mission management, the risk assessment, etc. There are several books authored to describe the design aspects of various areas, viz., propulsion, aerodynamics, structures, control, etc., but there is no book which presents space transportation system (STS) design in an integrated manner. This book attempts to fill this gap by addressing systems approach for STS design, highlighting the integrated design aspects, interactions between various subsystems and interdependencies. The main focus is towards the complex integrated design to arrive at an optimum, robust and cost effective space transportation system. The orbital mechanics of satellites including different coordinate frames, orbital perturbations and orbital transfers are explained. For launching the satellites to meet specific mission requirements, viz., payload/orbit, design considerations, giving step by step procedure are briefed. The selection methodology for launch vehicle configuration, its optimum staging and the factors which influence the vehicle performance are summarized. The influence of external, internal and dynamic operating environments experienced by the vehicle subsystems and the remedial measures needed are highlighted. The mission design strategies and their influence on the vehicle design process are elaborated. The various critical aspects of STS subsystems like flight mechanics, propulsion, structures and materials, thermal systems, stage auxiliary systems, navigation, guidance and control and the interdependencies and interactions between them are covered. The design guidelines, complexity of the flight environment and the reentry dynamics for the reentry missions are included. The book is not targeted as a design tool for any particular discipline or subsystem. Some of the design related equations or expressions are not attempted to derive from the first principle as this is beyond the scope of this book. However, the important analytical expressions, graphs and sketches which are essential to provide in-depth understanding for the design process as well as to understand the interactions between different subsystems are appropriately included.
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Page : 44 pages
File Size : 22,10 MB
Release : 1970
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Page : 1460 pages
File Size : 43,14 MB
Release : 1991
Category : Aeronautics
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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
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Page : 44 pages
File Size : 11,42 MB
Release : 1970
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Page : 36 pages
File Size : 35,63 MB
Release : 1970
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Page : 56 pages
File Size : 50,74 MB
Release : 1972
Category : Astronautical instruments
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Author : Alvar M. Kabe
Publisher : Academic Press
Page : 974 pages
File Size : 26,60 MB
Release : 2020-07-02
Category : Technology & Engineering
ISBN : 0128216212
The two-volume Structural Dynamics Fundamentals and Advanced Applications is a comprehensive work that encompasses the fundamentals of structural dynamics and vibration analysis, as well as advanced applications used on extremely large and complex systems. In Volume II, d'Alembert's Principle, Hamilton's Principle, and Lagrange's Equations are derived from fundamental principles. Development of large structural dynamic models and fluid/structure interaction are thoroughly covered. Responses to turbulence/gust, buffet, and static-aeroelastic loading encountered during atmospheric flight are addressed from fundamental principles to the final equations, including aeroelasticity. Volume II also includes a detailed discussion of mode survey testing, mode parameter identification, and analytical model adjustment. Analysis of time signals, including digitization, filtering, and transform computation is also covered. A comprehensive discussion of probability and statistics, including statistics of time series, small sample statistics, and the combination of responses whose statistical distributions are different, is included. Volume II concludes with an extensive chapter on continuous systems; including the classical derivations and solutions for strings, membranes, beams, and plates, as well as the derivation and closed form solutions for rotating disks and sloshing of fluids in rectangular and cylindrical tanks. Dr. Kabe's training and expertise are in structural dynamics and Dr. Sako's are in applied mathematics. Their collaboration has led to the development of first-of-a-kind methodologies and solutions to complex structural dynamics problems. Their experience and contributions encompass numerous past and currently operational launch and space systems. - The two-volume work was written with both practicing engineers and students just learning structural dynamics in mind - Derivations are rigorous and comprehensive, thus making understanding the material easier - Presents analysis methodologies adopted by the aerospace community to solve complex structural dynamics problems